Tuesday, February 22, 2011

G-force for More

Extended Acceleration
increases cruise velocity.
TimeDistance Velocity
1.0 Yr .38 LY .64 LY/Yr
1.2 Yr .51 LY .71 LY/Yr
1.4 Yr .66 LY .76 LY/Yr

G-force Accelerate for More than a Year
Total DistAccel TimeFinal
Velocity
Acceleration distanceCruise distanceCruise timeDecel timeTotal Time
DtAccVFindAccdCrutCrutDecT
LYdaysAU/day% cAULYLYYearsYearsYears
1 390.8 114.9466.38% 26,082 0.410.180.26 1.072.37
2 418.2 119.2268.85% 29,2400.46 1.081.561.143.82
3 447.5123.45 71.29% 32,741 0.52 1.962.76 1.235.17
4 478.8127.60 73.70% 36,6170.58 2.843.861.316.44
5512.3 131.67 76.04%40,901 0.65 3.714.871.407.64
6 548.2135.62 78.32%45,6250.72 4.56 5.821.508.78
7586.5139.43 80.52%50,827 0.80 5.396.701.619.86
8 627.6143.08 82.63%56,540.89 6.21 7.521.7110.90
9671.5 146.54 84.6362,816 0.99 7.018.291.8411.91
10 718.5149.81 86.52% 69,6831.10 7.809.01 1.9712.89
IV365.26(1.07)Dc[1 - (1 - Δ)tAcc]
ct +v(t)
ln(1-Δ)
DTtl - dAcc - dDec
dCru
VFin
tAcc 
365.26
tAcc + tCru + tDec
Definitions
  • D is total distance from our star, Sol, to destination. This table independently varies value from 1 to 10.
  • tAcc is acceleration duration from departure til start of cruise. This case study proposes a monotonic increase of this duration as shown. This method could shorten lengthy cruise times, but fuel consumption tradeoffs must be carefully considered.
  • Δ - Daily difference in spaceship's velocity is due to acceleration caused by constant g-force. We approximate this value: Δ = 86,400 g / c = .2826% c
  • VFin is final velocity achieved after applying g-force propulsion for tAcc duration.
    • vFin is also the maximum velocity achieved during the flight.
    • vFin is also cruise velocity; for this case study, it increases in correlation with acceleration duration.
  • dAcc is acceleration distance. It also increases in correlation with acceleration duration.
  • LY = 63,241 AU
  • dDec is deceleration distance; it equals acceleration distance.
  • dCru is cruise distance; it equals total distance minus distances for acceleration and deceleration.
  • tCru is cruise time as observed from the Earth.
  • tDec is deceleration time. Assuming consistent g-force, deceleration time equals acceleration time.
  • T is total time: acceleration + cruise + deceleration
AXIOM. Light speed is absolute and puts limits on interstellar travel. Even at light speed, interstellar flights take years for photons, virtually massless particles. Since human spaceships will contain large quantities of mass, the best we can hope for is to approach light speed; we can never attain it and certainly never surpass it.

ASSUMPTION-1. Self Contained Fuel. Prior to departure from Sol, notional spaceship will collect and carry sufficient fuel for planned propulsion phases to destination.

ASSUMPTION-2. Earthlike Gravity. We currently know two methods to achieve Earth like gravity on an interstellar vessel.

  • Constant G-force Acceleration. If an onboard propulsion system can increase ship's velocity by 9.80665 m/s for every second of "powered" flight, then ship's contents will feel a force equivalent to Terran gravity in the direction opposite to propulsion vector.
  • Centrifugal Force. If ship is not able to maintain g-force for entire flight, then the ship must spin so that contents feel forced against the inside of the outer hull. Thus, ship's shape should be cylindrical and rotate around its longitudinal axis; spin rate (usually given in degrees per second) will be inversely proportional to radius (as cylinder size increases, less spin rate is needed to maintain centripetal acceleration of 9.80665 m/s/s). Other pieces will present further details. (idea: insert figure with two g-force ships)

ASSUMPTION-3. Cruise Phase. TE considers it axiomatic that interstellar distances are so great that any interstellar voyage can easily require fuel consumption greater than 100% of ship's mass to power entire flight. Thus, the powered portions of flight (acceleration and deceleration) must be limited. Thus, an interstellar voyage must include a nonpowered cruise phase. Thus, TE assumes following flight profile.

  • Acceleration Phase. Ship starts off trip by accelerating at g-force for a given duration. TE arbitrarily chooses a base line duration of one year, but this acceleration duration can be extended within fuel limitations. During g-force acceleration, ship occupants will feel a gravity like force drawing them back to departure, Solar System; thus, "up" will be toward destination, and "down" will be toward Sol, departure star.
  • Cruise Phase. Due to fuel considerations, ship will stop propulsion after a planned duration and will maintain constant velocity. Fortunately, g-force acceleration for a year or more brings the ship to a significant portion of light speed, c, and reduces cruise duration from centuries to just years. Thus, ship will maintain constant velocity for entire cruise phase (majority of voyage). However, the cessation of propulsion will cause the ship to lose g-force from back of ship. To maintain Earth like gravity, occupants will have to reconfigure ship to maintain a controlled longtitudinal spin throughout the cruise phase. Thus, ship's spin will regain Earth like g-force by forcing contents against inside of outer hull.
  • Deceleration Phase. Ship will need to end this trip by slowing down from cruise speed to an operational speed. At a predetermined duration prior to arrival, ship will apply propulsion vector against direction of flight. While acceleration phase directed exhaust particles toward Sol, departure; the deceleration propulsion vector will point in opposite direction, toward destination. Now, "up" will now be in the direction of Sol which is retreating from the ship, and "down" will be toward destination, which is getting closer.

Closest Destinations.
DestinationAccel TimeFinal
Velocity
Acceleration distanceCruise distanceCruise timeDecel timeTotal Time
StarDtAccVFindAccdCrutCrutDecT
NameLYdaysAU/day% cAULYLYYearsYearsYears
Alpha Centauri4.365 490.8 129.97 75.06% 39,047 0.62 3.13 4.17 1.346.86
Barnard's Star5.963 546.8 136.30 78.72% 46,512 0.74 4.49 5.71 1.50 8.70
Wolf7.786 618.6 143.08 82.63% 56,547 0.89 6.00 7.26 1.69 10.65
Lalande8.291 640.1 144.85 83.66% 59,642 0.94 6.40 7.66 1.7511.16
Sirius8.583 652.8 145.86 84.24% 61,499 0.97 6.64 7.88 1.7911.45
Luyten8.728 659.3 146.35 84.52% 62,439 0.99 6.75 7.99 1.8011.60
Ross9.681 703.2 149.48 86.33% 68,935 1.09 7.50 8.69 1.9312.54
ObservedGivenc[1 - (1 - Δ)tAcc]
c= 173.15 AU/dy
ct +v(t)
ln(1-Δ)
DTtl - dAcc - dDec
dCru
VFin
tAcc
365.26
tAcc + tCru + tDec

Thursday, February 17, 2011

G-force Limitations

1st, TECHNOLOGY. We have yet to design, build and operate a spaceship with a particle accelerator as the propulsion system; thus, the most compelling limit will be the transition from notional to actual. Of the numerous design tasks, an extremely difficult one will involves enormous energy to bring exhaust particles to near light speeds. Once solved, the increased mass and speed of the exhaust fuel flow (ffExh) will product an enormous momentum to propel the spaceship at g-force acceleration throughout powered flight. Throughout these volumes, several tables show that the higher the particle exhaust speed, the lower the quantity of original fuel mass (fuel flow per sec, ffsec) needed to propel the ship at g-force. This means that less fuel needs to exit the spaceship for same distance traveled. HOWEVER, this increased momentum comes at a cost; much more energy is required by spaceship to accelerate the particles to these near light speeds.
2nd, FINITE RANGE. Above g-force requires fuel consumption, and our space vehicle will eventually deplete the fuel supply. Further considerations:
%TOGW Limit is ½ ship’s mass. Percentage of ship’s TakeOff Gross Weight (TOGW is also known as initial ship’s mass) must be used for fuel with the rest needed for infrastructure and payload. Thot exp assumes 50%, but it could range from 10% to 90%.
Return flight mandates a reserve. Cautious planning leads us to assume no refueling at destination or anywhere else along the flight path. Thought experiment assumes another 50% reduction to plan for return flight.
Efficiency factor needs a margin. It's safe to assume that our initial flight design will not be perfect. Even if it was, we still have to consider energy needs for life support, and many other auxilliary energy requirements.

Above factors lead us to determe total propulsion time (tp) from effectively converting 1/8th of the ship’s TOGW to kinetic energy. A further range limitation comes from the flight profile required to maintain g-force throughout the voyage.

Flight Profile. Accelerate for ½ tp. Another range limitation comes from thot exp’s self imposed flight profile where the ship accelerates to half distance, then decelerates for remaining half. We’ve chosen this profile as best way to maintain g-force throughout the trip. We could possibly improve the range by accelerating perhaps 90% of the distance then decelerating at a much greater force for remaining 10% of distance. However, this much greater force would greatly exceed Earth like gravity and thot exp assumes this to be undesireable.
3rd. STELLAR DISTANCES. Our finite range seems to keep getting whacked by above considerations; however, the near light speed of exhaust particles impact so much specific impulse that interplanetary space travel is easily accomplished with considerable margin. Consider above interplanetary table, the most demanding range (Kuiper Belt) is easily covered by the least capable row in the interstellar table (where n= 2).

On the other hand, margin is definitely not there for interstellar travel. Consider the most generous table in the interstellar table (exhaust particle traveling so fast that relativistic effects grow it 11 times mass of same particles at relative rest with the spacecraft). Conservatively, resulting momentum gives spacecraft a range of 329 days of acceleration to take us to 1/3 of one LY; another 329 days of deceleration would take us to .64 LY, the entire distinace is not even close to the Oort Cloud, edge of our Solar System.
Thus far, our notional spacecraft hasn't made any significant progress toward our nearest stellar neighber; yet, our notional spacecraft has already exhausted available fuel. Thus, we must now use reserve fuel to return back to departure point, while still far short of our goal.
4th. RELATIVISTIC PARADOX. Consider an extreme scenario from one of Robert Heinlein's novels, which elaborates on the "twin paradox". Two identical twins grow up together then separate, where one twin accelerates to near light speed, then travels on an interstellar journey for a few years. The traveling twin ages a few years and eventually returns to Earth as still a young man. Upon his return, he's amazed to discover that his meager savings has made him very wealthy and his twin has become an old man; so old, that he marries his twin's great-granddaughter. This fanciful story illustrates that relativistic effects could become very pronounced; thus, this thought experiment assumes that near light speed travel will be accomplished in a carefully controlled manner. For example, initial trips to Alpha Centauri might attain a cruise velocity of perhaps .5c, observing results, then incrementing subsequent trip's cruise speed to perhaps .51c, and so on. copythis

Wednesday, February 02, 2011

Marsonance Table: 2 Cyclers

For resonance, 
cycler orbit has same period (P) as Mars.
PCy = 1.88 yr = 687 days = P
From Kepler’s Third Law, 
P2  a3
thus, the primary orbital element,
 semi-major axis (a),
must be same for both cycler and Mars.
aCy = 1.88 AU = a



For useful rendezvous, 
cycler orbit persistently intercepts Mars orbit.
THEREFORE, orbits must differ,
and all other orbital elements likely differ.
These include: aphelion (Q), perihelion (q), eccentricity (e), semi-latis rectum (and respective area (A).
Mars
Angle
Mars Radius Cum
Area
Cum
Time
Mars
Incr.
Time
Earth
Angle
.Cycler1.
Angle
Cycler1
Radius
Incr.
Angle
Cycler
Incr.
Time
Incr.
Angle
.Cycler2.
Angle
Cycler2
Radius
θ R A T Δt θ θC1 RC1 ∆θC1 ΔtCy ∆θC2 θC2 RC2
Deg AU AU2 days days Deg Deg AU Deg days Deg Deg AU
0 ⁰ 1.3814 0.0000 0.0 1.58 0.00 ⁰ 124.24 ⁰ 1.5156 0.69 ⁰ 1.58 0.68 ⁰ 235.28 ⁰ 1.5243
1 ⁰ 1.3814 0.0167 1.6 1.58 1.55 ⁰ 124.92 ⁰ 1.5281 0.68 ⁰ 1.58 0.69 ⁰ 235.97 ⁰ 1.5117
2 ⁰ 1.3815 0.0333 3.2 1.58 3.11 ⁰ 125.60 ⁰ 1.5406 0.67 ⁰ 1.58 0.70 ⁰ 236.67 ⁰ 1.4990
3 ⁰ 1.3816 0.0500 4.7 1.58 4.66 ⁰ 126.26 ⁰ 1.5529 0.66 ⁰ 1.58 0.71 ⁰ 237.38 ⁰ 1.4862
4 ⁰ 1.3817 0.0666 6.3 1.58 6.21 ⁰ 126.91 ⁰ 1.5652 0.65 ⁰ 1.58 0.72 ⁰ 238.10 ⁰ 1.4733
5 ⁰ 1.3818 0.0833 7.9 1.58 7.77 ⁰ 127.54 ⁰ 1.5773 0.64 ⁰ 1.58 0.73 ⁰ 238.83 ⁰ 1.4603
6 ⁰ 1.3820 0.0999 9.5 1.58 9.32 ⁰ 128.18 ⁰ 1.5893 0.63 ⁰ 1.58 0.75 ⁰ 239.58 ⁰ 1.4473
7 ⁰ 1.3823 0.1166 11.0 1.58 10.87 ⁰ 128.80 ⁰ 1.6013 0.62 ⁰ 1.58 0.76 ⁰ 240.34 ⁰ 1.4341
8 ⁰ 1.3825 0.1333 12.6 1.58 12.43 ⁰ 129.41 ⁰ 1.6131 0.61 ⁰ 1.58 0.78 ⁰ 241.12 ⁰ 1.4208
9 ⁰ 1.3829 0.1500 14.2 1.58 13.98 ⁰ 130.02 ⁰ 1.6249 0.60 ⁰ 1.58 0.79 ⁰ 241.91 ⁰ 1.4074
10 ⁰ 1.3832 0.1667 15.8 1.58 15.54 ⁰ 130.61 ⁰ 1.6365 0.60 ⁰ 1.58 0.80 ⁰ 242.71 ⁰ 1.3939
11 ⁰ 1.3836 0.1834 17.3 1.58 17.10 ⁰ 131.20 ⁰ 1.6481 0.58 ⁰ 1.58 0.82 ⁰ 243.53 ⁰ 1.3803
12 ⁰ 1.3840 0.2001 18.9 1.58 18.66 ⁰ 131.77 ⁰ 1.6595 0.58 ⁰ 1.58 0.84 ⁰ 244.37 ⁰ 1.3666
13 ⁰ 1.3844 0.2168 20.5 1.58 20.21 ⁰ 132.34 ⁰ 1.6708 0.57 ⁰ 1.58 0.85 ⁰ 245.22 ⁰ 1.3528
14 ⁰ 1.3849 0.2335 22.1 1.58 21.77 ⁰ 132.91 ⁰ 1.6820 0.56 ⁰ 1.58 0.88 ⁰ 246.10 ⁰ 1.3389
15 ⁰ 1.3854 0.2503 23.7 1.58 23.34 ⁰ 133.46 ⁰ 1.6931 0.56 ⁰ 1.58 0.89 ⁰ 246.99 ⁰ 1.3249
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
16 ⁰ 1.3860 0.2670 25.3 1.59 24.90 ⁰ 134.01 ⁰ 1.7042 0.55 ⁰ 1.59 0.92 ⁰ 247.91 ⁰ 1.3107
17 ⁰ 1.3866 0.2838 26.8 1.59 26.46 ⁰ 134.56 ⁰ 1.7152 0.55 ⁰ 1.59 0.94 ⁰ 248.84 ⁰ 1.2964
18 ⁰ 1.3872 0.3006 28.4 1.59 28.03 ⁰ 135.10 ⁰ 1.7261 0.54 ⁰ 1.59 0.96 ⁰ 249.80 ⁰ 1.2821
19 ⁰ 1.3879 0.3174 30.0 1.59 29.59 ⁰ 135.63 ⁰ 1.7369 0.53 ⁰ 1.59 0.98 ⁰ 250.78 ⁰ 1.2676
20 ⁰ 1.3886 0.3342 31.6 1.59 31.16 ⁰ 136.15 ⁰ 1.7476 0.53 ⁰ 1.59 1.00 ⁰ 251.78 ⁰ 1.2531
21 ⁰ 1.3893 0.3510 33.2 1.59 32.73 ⁰ 136.67 ⁰ 1.7582 0.52 ⁰ 1.59 1.02 ⁰ 252.80 ⁰ 1.2386
22 ⁰ 1.3900 0.3679 34.8 1.59 34.30 ⁰ 137.18 ⁰ 1.7687 0.51 ⁰ 1.59 1.05 ⁰ 253.85 ⁰ 1.2239
23 ⁰ 1.3908 0.3848 36.4 1.60 35.87 ⁰ 137.69 ⁰ 1.7792 0.51 ⁰ 1.60 1.08 ⁰ 254.93 ⁰ 1.2090
24 ⁰ 1.3917 0.4017 38.0 1.60 37.45 ⁰ 138.19 ⁰ 1.7895 0.50 ⁰ 1.60 1.11 ⁰ 256.04 ⁰ 1.1941
25 ⁰ 1.3925 0.4186 39.6 1.60 39.03 ⁰ 138.69 ⁰ 1.7997 0.50 ⁰ 1.60 1.14 ⁰ 257.18 ⁰ 1.1790
26 ⁰ 1.3934 0.4355 41.2 1.60 40.61 ⁰ 139.18 ⁰ 1.8099 0.49 ⁰ 1.60 1.16 ⁰ 258.34 ⁰ 1.1639
27 ⁰ 1.3944 0.4525 42.8 1.60 42.19 ⁰ 139.67 ⁰ 1.8199 0.48 ⁰ 1.60 1.20 ⁰ 259.54 ⁰ 1.1488
28 ⁰ 1.3954 0.4694 44.4 1.61 43.77 ⁰ 140.15 ⁰ 1.8299 0.49 ⁰ 1.61 1.24 ⁰ 260.78 ⁰ 1.1334
29 ⁰ 1.3964 0.4864 46.0 1.61 45.35 ⁰ 140.63 ⁰ 1.8399 0.48 ⁰ 1.61 1.27 ⁰ 262.05 ⁰ 1.1180
30 ⁰ 1.3974 0.5035 47.6 1.61 46.94 ⁰ 141.102 ⁰ 1.8497 0.47 ⁰ 1.61 1.31 ⁰ 263.36 ⁰ 1.1027
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
31 ⁰ 1.3985 0.5205 49.2 1.61 48.53 ⁰ 141.57 ⁰ 1.8594 0.47 ⁰ 1.61 1.35 ⁰ 264.70 ⁰ 1.0871
32 ⁰ 1.3996 0.5376 50.9 1.62 50.12 ⁰ 142.04 ⁰ 1.8691 0.47 ⁰ 1.62 1.40 ⁰ 266.10 ⁰ 1.0715
33 ⁰ 1.4007 0.5547 52.5 1.62 51.72 ⁰ 142.50 ⁰ 1.8787 0.46 ⁰ 1.62 1.44 ⁰ 267.53 ⁰ 1.0559
34 ⁰ 1.4019 0.5718 54.1 1.62 53.32 ⁰ 142.96 ⁰ 1.8881 0.46 ⁰ 1.62 1.48 ⁰ 269.01 ⁰ 1.0402
35 ⁰ 1.4031 0.5890 55.7 1.62 54.92 ⁰ 143.41 ⁰ 1.8975 0.45 ⁰ 1.62 1.52 ⁰ 270.53 ⁰ 1.0246
36 ⁰ 1.4043 0.6062 57.3 1.63 56.52 ⁰ 143.86 ⁰ 1.9069 0.45 ⁰ 1.63 1.58 ⁰ 272.11 ⁰ 1.0088
37 ⁰ 1.4056 0.6234 59.0 1.63 58.13 ⁰ 144.31 ⁰ 1.9161 0.45 ⁰ 1.63 1.63 ⁰ 273.74 ⁰ 0.9931
38 ⁰ 1.4069 0.6407 60.6 1.63 59.74 ⁰ 144.75 ⁰ 1.9252 0.44 ⁰ 1.63 1.68 ⁰ 275.42 ⁰ 0.9774
39 ⁰ 1.4082 0.6580 62.2 1.64 61.35 ⁰ 145.19 ⁰ 1.9343 0.44 ⁰ 1.64 1.74 ⁰ 277.17 ⁰ 0.9617
40 ⁰ 1.4096 0.6753 63.9 1.64 62.96 ⁰ 145.63 ⁰ 1.9433 0.44 ⁰ 1.64 1.80 ⁰ 278.97 ⁰ 0.9460
41 ⁰ 1.4110 0.6927 65.5 1.64 64.58 ⁰ 146.06 ⁰ 1.9522 0.43 ⁰ 1.64 1.86 ⁰ 280.83 ⁰ 0.9305
42 ⁰ 1.4124 0.7100 67.2 1.65 66.20 ⁰ 146.49 ⁰ 1.9610 0.43 ⁰ 1.65 1.94 ⁰ 282.77 ⁰ 0.9149
43 ⁰ 1.4138 0.7275 68.8 1.65 67.83 ⁰ 146.92 ⁰ 1.9698 0.43 ⁰ 1.65 2.01 ⁰ 284.78 ⁰ 0.8994
44 ⁰ 1.4153 0.7449 70.5 1.65 69.46 ⁰ 147.34 ⁰ 1.9785 0.42 ⁰ 1.65 2.08 ⁰ 286.86 ⁰ 0.8840
45 ⁰ 1.4168 0.7624 72.1 1.66 71.09 ⁰ 147.77 ⁰ 1.9870 0.42 ⁰ 1.66 2.16 ⁰ 289.02 ⁰ 0.8688
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
46 ⁰ 1.4184 0.7800 73.8 1.66 72.72 ⁰ 148.19 ⁰ 1.9955 0.42 ⁰ 1.66 2.25 ⁰ 291.26 ⁰ 0.8537
47 ⁰ 1.4200 0.7975 75.4 1.66 74.36 ⁰ 148.60 ⁰ 2.0040 0.42 ⁰ 1.66 2.32 ⁰ 293.59 ⁰ 0.8389
48 ⁰ 1.4216 0.8152 77.1 1.67 76.00 ⁰ 149.02 ⁰ 2.0123 0.41 ⁰ 1.67 2.42 ⁰ 296.00 ⁰ 0.8243
49 ⁰ 1.4232 0.8328 78.8 1.67 77.65 ⁰ 149.43 ⁰ 2.0206 0.41 ⁰ 1.67 2.51 ⁰ 298.51 ⁰ 0.8099
50 ⁰ 1.4249 0.8505 80.5 1.67 79.30 ⁰ 149.83 ⁰ 2.0287 0.41 ⁰ 1.67 2.60 ⁰ 301.11 ⁰ 0.7959
51 ⁰ 1.4266 0.8683 82.1 1.68 80.95 ⁰ 150.24 ⁰ 2.0368 0.41 ⁰ 1.68 2.70 ⁰ 303.81 ⁰ 0.7822
52 ⁰ 1.4283 0.8860 83.8 1.68 82.61 ⁰ 150.65 ⁰ 2.0448 0.40 ⁰ 1.68 2.80 ⁰ 306.61 ⁰ 0.7689
53 ⁰ 1.4300 0.9039 85.5 1.69 84.27 ⁰ 151.05 ⁰ 2.0528 0.40 ⁰ 1.69 2.91 ⁰ 309.52 ⁰ 0.7560
54 ⁰ 1.4318 0.9217 87.2 1.69 85.94 ⁰ 151.45 ⁰ 2.0606 0.40 ⁰ 1.69 3.01 ⁰ 312.53 ⁰ 0.7437
55 ⁰ 1.4336 0.9396 88.9 1.69 87.61 ⁰ 151.85 ⁰ 2.0684 0.40 ⁰ 1.69 3.11 ⁰ 315.64 ⁰ 0.7320
56 ⁰ 1.4355 0.9576 90.6 1.70 89.28 ⁰ 152.24 ⁰ 2.0761 0.40 ⁰ 1.70 3.22 ⁰ 318.86 ⁰ 0.7209
57 ⁰ 1.4373 0.9756 92.3 1.70 90.96 ⁰ 152.64 ⁰ 2.0837 0.39 ⁰ 1.70 3.32 ⁰ 322.18 ⁰ 0.7105
58 ⁰ 1.4392 0.9937 94.0 1.71 92.65 ⁰ 153.03 ⁰ 2.0912 0.39 ⁰ 1.71 3.43 ⁰ 325.61 ⁰ 0.7007
59 ⁰ 1.4411 1.0118 95.7 1.71 94.33 ⁰ 153.42 ⁰ 2.0986 0.39 ⁰ 1.71 3.52 ⁰ 329.13 ⁰ 0.6919
60 ⁰ 1.4430 1.0299 97.4 1.72 96.03 ⁰ 153.81 ⁰ 2.1060 0.39 ⁰ 1.72 3.64 ⁰ 332.78 ⁰ 0.6838
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
61 ⁰ 1.4450 1.0481 99.2 1.72 97.72 ⁰ 154.19 ⁰ 2.1133 0.39 ⁰ 1.72 3.71 ⁰ 336.49 ⁰ 0.6767
62 ⁰ 1.4470 1.0663 100.9 1.73 99.42 ⁰ 154.58 ⁰ 2.1205 0.39 ⁰ 1.73 3.82 ⁰ 340.31 ⁰ 0.6705
63 ⁰ 1.4490 1.0846 102.6 1.73 101.13 ⁰ 154.96 ⁰ 2.1276 0.38 ⁰ 1.73 3.88 ⁰ 344.19 ⁰ 0.6654
64 ⁰ 1.4510 1.1030 104.3 1.74 102.84 ⁰ 155.35 ⁰ 2.1347 0.38 ⁰ 1.74 3.97 ⁰ 348.16 ⁰ 0.6614
65 ⁰ 1.4531 1.1214 106.1 1.74 104.56 ⁰ 155.73 ⁰ 2.1417 0.38 ⁰ 1.74 4.00 ⁰ 352.16 ⁰ 0.6585
66 ⁰ 1.4551 1.1398 107.8 1.75 106.28 ⁰ 156.11 ⁰ 2.1486 0.38 ⁰ 1.75 4.05 ⁰ 356.20 ⁰ 0.6568
67 ⁰ 1.4572 1.1583 109.6 1.75 108.00 ⁰ 156.49 ⁰ 2.1554 0.38 ⁰ 1.75 4.06 ⁰ 0.25 ⁰ 0.6563
68 ⁰ 1.4594 1.1769 111.3 1.76 109.73 ⁰ 156.87 ⁰ 2.1621 0.38 ⁰ 1.76 4.07 ⁰ 4.33 ⁰ 0.6570
69 ⁰ 1.4615 1.1955 113.1 1.76 111.47 ⁰ 157.24 ⁰ 2.1687 0.38 ⁰ 1.76 4.07 ⁰ 8.40 ⁰ 0.6589
70 ⁰ 1.4637 1.2142 114.9 1.77 113.21 ⁰ 157.62 ⁰ 2.1753 0.38 ⁰ 1.77 4.07 ⁰ 12.48 ⁰ 0.6620
71 ⁰ 1.4658 1.2329 116.6 1.77 114.95 ⁰ 157.99 ⁰ 2.1818 0.37 ⁰ 1.77 4.02 ⁰ 16.50 ⁰ 0.6663
72 ⁰ 1.4680 1.2517 118.4 1.78 116.70 ⁰ 158.36 ⁰ 2.1882 0.37 ⁰ 1.78 3.98 ⁰ 20.48 ⁰ 0.6717
73 ⁰ 1.4703 1.2705 120.2 1.78 118.46 ⁰ 158.74 ⁰ 2.1944 0.37 ⁰ 1.78 3.91 ⁰ 24.39 ⁰ 0.6783
74 ⁰ 1.4725 1.2894 122.0 1.79 120.22 ⁰ 159.11 ⁰ 2.2007 0.37 ⁰ 1.79 3.84 ⁰ 28.23 ⁰ 0.6859
75 ⁰ 1.4748 1.3084 123.8 1.79 121.99 ⁰ 159.48 ⁰ 2.2068 0.37 ⁰ 1.79 3.77 ⁰ 32.00 ⁰ 0.6946
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
76 ⁰ 1.4770 1.3274 125.6 1.80 123.76 ⁰ 159.84 ⁰ 2.2128 0.37 ⁰ 1.80 3.68 ⁰ 35.68 ⁰ 0.7043
77 ⁰ 1.4793 1.3464 127.4 1.80 125.54 ⁰ 160.21 ⁰ 2.2187 0.37 ⁰ 1.80 3.58 ⁰ 39.26 ⁰ 0.7148
78 ⁰ 1.4816 1.3656 129.2 1.81 127.32 ⁰ 160.58 ⁰ 2.2246 0.37 ⁰ 1.81 3.49 ⁰ 42.74 ⁰ 0.7263
79 ⁰ 1.4840 1.3848 131.0 1.82 129.11 ⁰ 160.94 ⁰ 2.2304 0.37 ⁰ 1.82 3.39 ⁰ 46.13 ⁰ 0.7386
80 ⁰ 1.4863 1.4040 132.8 1.82 130.91 ⁰ 161.31 ⁰ 2.2361 0.37 ⁰ 1.82 3.29 ⁰ 49.42 ⁰ 0.7516
81 ⁰ 1.4887 1.4233 134.6 1.83 132.71 ⁰ 161.68 ⁰ 2.2417 0.37 ⁰ 1.83 3.19 ⁰ 52.61 ⁰ 0.7654
82 ⁰ 1.4910 1.4427 136.5 1.83 134.51 ⁰ 162.04 ⁰ 2.2472 0.36 ⁰ 1.83 3.06 ⁰ 55.67 ⁰ 0.7796
83 ⁰ 1.4934 1.4621 138.3 1.84 136.32 ⁰ 162.40 ⁰ 2.2526 0.36 ⁰ 1.84 2.98 ⁰ 58.64 ⁰ 0.7946
84 ⁰ 1.4958 1.4816 140.2 1.84 138.14 ⁰ 162.77 ⁰ 2.2580 0.36 ⁰ 1.84 2.86 ⁰ 61.50 ⁰ 0.8099
85 ⁰ 1.4982 1.5012 142.0 1.85 139.97 ⁰ 163.13 ⁰ 2.2632 0.36 ⁰ 1.85 2.77 ⁰ 64.27 ⁰ 0.8258
86 ⁰ 1.5006 1.5208 143.9 1.86 141.79 ⁰ 163.49 ⁰ 2.2683 0.36 ⁰ 1.86 2.68 ⁰ 66.94 ⁰ 0.8422
87 ⁰ 1.5031 1.5405 145.7 1.86 143.63 ⁰ 163.85 ⁰ 2.2734 0.36 ⁰ 1.86 2.58 ⁰ 69.52 ⁰ 0.8589
88 ⁰ 1.5055 1.5602 147.6 1.87 145.47 ⁰ 164.21 ⁰ 2.2784 0.36 ⁰ 1.87 2.49 ⁰ 72.01 ⁰ 0.8760
89 ⁰ 1.5080 1.5800 149.5 1.87 147.32 ⁰ 164.57 ⁰ 2.2832 0.36 ⁰ 1.87 2.39 ⁰ 74.40 ⁰ 0.8932
90 ⁰ 1.5104 1.5999 151.4 1.88 149.17 ⁰ 164.93 ⁰ 2.2880 0.36 ⁰ 1.88 2.31 ⁰ 76.71 ⁰ 0.9108
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
91 ⁰ 1.5129 1.6198 153.2 1.89 151.03 ⁰ 165.29 ⁰ 2.2927 0.36 ⁰ 1.89 2.23 ⁰ 78.94 ⁰ 0.9286
92 ⁰ 1.5154 1.6399 155.1 1.89 152.90 ⁰ 165.65 ⁰ 2.2973 0.36 ⁰ 1.89 2.16 ⁰ 81.10 ⁰ 0.9466
93 ⁰ 1.5178 1.6599 157.0 1.90 154.77 ⁰ 166.01 ⁰ 2.3017 0.36 ⁰ 1.90 2.08 ⁰ 83.18 ⁰ 0.9648
94 ⁰ 1.5203 1.6801 158.9 1.91 156.65 ⁰ 166.37 ⁰ 2.3061 0.36 ⁰ 1.91 2.02 ⁰ 85.20 ⁰ 0.9831
95 ⁰ 1.5228 1.7003 160.8 1.91 158.53 ⁰ 166.73 ⁰ 2.3104 0.36 ⁰ 1.91 1.94 ⁰ 87.14 ⁰ 1.0015
96 ⁰ 1.5253 1.7205 162.8 1.92 160.42 ⁰ 167.09 ⁰ 2.3146 0.36 ⁰ 1.92 1.88 ⁰ 89.02 ⁰ 1.0200
97 ⁰ 1.5278 1.7409 164.7 1.92 162.32 ⁰ 167.45 ⁰ 2.3187 0.36 ⁰ 1.92 1.82 ⁰ 90.83 ⁰ 1.0386
98 ⁰ 1.5303 1.7613 166.6 1.93 164.22 ⁰ 167.81 ⁰ 2.3227 0.36 ⁰ 1.93 1.76 ⁰ 92.59 ⁰ 1.0572
99 ⁰ 1.5328 1.7817 168.6 1.94 166.13 ⁰ 168.17 ⁰ 2.3266 0.36 ⁰ 1.94 1.71 ⁰ 94.30 ⁰ 1.0759
100 ⁰ 1.5353 1.8023 170.5 1.94 168.04 ⁰ 168.52 ⁰ 2.3304 0.36 ⁰ 1.94 1.65 ⁰ 95.94 ⁰ 1.0945
101 ⁰ 1.5378 1.8229 172.4 1.95 169.96 ⁰ 168.88 ⁰ 2.3341 0.36 ⁰ 1.95 1.60 ⁰ 97.54 ⁰ 1.1132
102 ⁰ 1.5403 1.8436 174.4 1.96 171.89 ⁰ 169.24 ⁰ 2.3377 0.36 ⁰ 1.96 1.56 ⁰ 99.10 ⁰ 1.1319
103 ⁰ 1.5428 1.8643 176.4 1.96 173.82 ⁰ 169.60 ⁰ 2.3412 0.36 ⁰ 1.96 1.51 ⁰ 100.61 ⁰ 1.1506
104 ⁰ 1.5453 1.8851 178.3 1.97 175.76 ⁰ 169.96 ⁰ 2.3445 0.36 ⁰ 1.97 1.46 ⁰ 102.07 ⁰ 1.1692
105 ⁰ 1.5478 1.9060 180.3 1.97 177.71 ⁰ 170.32 ⁰ 2.3478 0.36 ⁰ 1.97 1.42 ⁰ 103.49 ⁰ 1.1877
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
106 ⁰ 1.5503 1.9269 182.3 1.98 179.66 ⁰ 170.68 ⁰ 2.3510 0.36 ⁰ 1.98 1.38 ⁰ 104.87 ⁰ 1.2063
107 ⁰ 1.5528 1.9479 184.3 1.99 181.62 ⁰ 171.04 ⁰ 2.3540 0.36 ⁰ 1.99 1.35 ⁰ 106.22 ⁰ 1.2248
108 ⁰ 1.5553 1.9690 186.3 1.99 183.59 ⁰ 171.40 ⁰ 2.3569 0.36 ⁰ 1.99 1.31 ⁰ 107.53 ⁰ 1.2431
109 ⁰ 1.5578 1.9901 188.3 2.00 185.56 ⁰ 171.76 ⁰ 2.3598 0.36 ⁰ 2.00 1.27 ⁰ 108.80 ⁰ 1.2615
110 ⁰ 1.5603 2.0114 190.3 2.01 187.53 ⁰ 172.12 ⁰ 2.3625 0.36 ⁰ 2.01 1.25 ⁰ 110.05 ⁰ 1.2798
111 ⁰ 1.5627 2.0326 192.3 2.01 189.52 ⁰ 172.48 ⁰ 2.3651 0.36 ⁰ 2.01 1.21 ⁰ 111.26 ⁰ 1.2979
112 ⁰ 1.5652 2.0540 194.3 2.02 191.51 ⁰ 172.84 ⁰ 2.3676 0.36 ⁰ 2.02 1.18 ⁰ 112.44 ⁰ 1.3160
113 ⁰ 1.5676 2.0754 196.3 2.03 193.51 ⁰ 173.20 ⁰ 2.3700 0.36 ⁰ 2.03 1.16 ⁰ 113.59 ⁰ 1.3340
114 ⁰ 1.5701 2.0969 198.4 2.03 195.51 ⁰ 173.56 ⁰ 2.3722 0.36 ⁰ 2.03 1.13 ⁰ 114.72 ⁰ 1.3519
115 ⁰ 1.5725 2.1184 200.4 2.04 197.52 ⁰ 173.92 ⁰ 2.3744 0.36 ⁰ 2.04 1.10 ⁰ 115.82 ⁰ 1.3697
116 ⁰ 1.5749 2.1400 202.4 2.04 199.53 ⁰ 174.28 ⁰ 2.3764 0.36 ⁰ 2.04 1.07 ⁰ 116.89 ⁰ 1.3873
117 ⁰ 1.5773 2.1617 204.5 2.05 201.55 ⁰ 174.65 ⁰ 2.3783 0.36 ⁰ 2.05 1.05 ⁰ 117.95 ⁰ 1.4049
118 ⁰ 1.5797 2.1834 206.6 2.06 203.58 ⁰ 175.01 ⁰ 2.3801 0.37 ⁰ 2.06 1.03 ⁰ 118.98 ⁰ 1.4224
119 ⁰ 1.5821 2.2053 208.6 2.06 205.61 ⁰ 175.38 ⁰ 2.3818 0.36 ⁰ 2.06 1.01 ⁰ 119.99 ⁰ 1.4397
120 ⁰ 1.5844 2.2271 210.7 2.07 207.65 ⁰ 175.74 ⁰ 2.3833 0.37 ⁰ 2.07 0.99 ⁰ 120.97 ⁰ 1.4569
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
121 ⁰ 1.5867 2.2491 212.8 2.08 209.70 ⁰ 176.11 ⁰ 2.3847 0.37 ⁰ 2.08 0.97 ⁰ 121.94 ⁰ 1.4740
122 ⁰ 1.5891 2.2711 214.8 2.08 211.75 ⁰ 176.47 ⁰ 2.3860 0.37 ⁰ 2.08 0.95 ⁰ 122.89 ⁰ 1.4910
123 ⁰ 1.5914 2.2931 216.9 2.09 213.81 ⁰ 176.84 ⁰ 2.3872 0.37 ⁰ 2.09 0.93 ⁰ 123.82 ⁰ 1.5078
124 ⁰ 1.5937 2.3153 219.0 2.09 215.87 ⁰ 177.21 ⁰ 2.3883 0.37 ⁰ 2.09 0.91 ⁰ 124.73 ⁰ 1.5245
125 ⁰ 1.5959 2.3375 221.1 2.10 217.94 ⁰ 177.58 ⁰ 2.3892 0.37 ⁰ 2.10 0.89 ⁰ 125.62 ⁰ 1.5411
126 ⁰ 1.5982 2.3597 223.2 2.11 220.02 ⁰ 177.95 ⁰ 2.3900 0.37 ⁰ 2.11 0.88 ⁰ 126.50 ⁰ 1.5575
127 ⁰ 1.6004 2.3820 225.3 2.11 222.10 ⁰ 178.31 ⁰ 2.3906 0.37 ⁰ 2.11 0.86 ⁰ 127.36 ⁰ 1.5738
128 ⁰ 1.6026 2.4044 227.5 2.12 224.18 ⁰ 178.69 ⁰ 2.3912 0.37 ⁰ 2.12 0.85 ⁰ 128.21 ⁰ 1.5899
129 ⁰ 1.6047 2.4269 229.6 2.12 226.28 ⁰ 179.06 ⁰ 2.3916 0.37 ⁰ 2.12 0.79 ⁰ 129.00 ⁰ 1.6052
130 ⁰ 1.6069 2.4494 231.7 2.13 228.37 ⁰ 179.43 ⁰ 2.3919 0.37 ⁰ 2.13 0.81 ⁰ 129.82 ⁰ 1.6210
131 ⁰ 1.6090 2.4719 233.8 2.13 230.48 ⁰ 179.80 ⁰ 2.3920 0.37 ⁰ 2.13 0.80 ⁰ 130.62 ⁰ 1.6367
132 ⁰ 1.6111 2.4946 236.0 2.14 232.59 ⁰ 180.17 ⁰ 2.3920 0.37 ⁰ 2.14 0.79 ⁰ 131.41 ⁰ 1.6523
133 ⁰ 1.6132 2.5172 238.1 2.15 234.70 ⁰ 180.55 ⁰ 2.3919 0.38 ⁰ 2.15 0.78 ⁰ 132.19 ⁰ 1.6678
134 ⁰ 1.6152 2.5400 240.3 2.15 236.82 ⁰ 180.93 ⁰ 2.3916 0.38 ⁰ 2.15 0.77 ⁰ 132.96 ⁰ 1.6831
135 ⁰ 1.6172 2.5628 242.4 2.16 238.95 ⁰ 181.30 ⁰ 2.3912 0.38 ⁰ 2.16 0.75 ⁰ 133.72 ⁰ 1.6983
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
136 ⁰ 1.6192 2.5856 244.6 2.16 241.08 ⁰ 181.68 ⁰ 2.3906 0.38 ⁰ 2.16 0.74 ⁰ 134.46 ⁰ 1.7132
137 ⁰ 1.6212 2.6085 246.8 2.17 243.21 ⁰ 182.06 ⁰ 2.3900 0.38 ⁰ 2.17 0.73 ⁰ 135.19 ⁰ 1.7281
138 ⁰ 1.6231 2.6315 248.9 2.17 245.35 ⁰ 182.44 ⁰ 2.3891 0.38 ⁰ 2.17 0.72 ⁰ 135.91 ⁰ 1.7427
139 ⁰ 1.6250 2.6545 251.1 2.18 247.50 ⁰ 182.83 ⁰ 2.3882 0.38 ⁰ 2.18 0.71 ⁰ 136.62 ⁰ 1.7573
140 ⁰ 1.6268 2.6776 253.3 2.18 249.65 ⁰ 183.21 ⁰ 2.3871 0.38 ⁰ 2.18 0.70 ⁰ 137.32 ⁰ 1.7716
141 ⁰ 1.6286 2.7007 255.5 2.19 251.81 ⁰ 183.59 ⁰ 2.3858 0.38 ⁰ 2.19 0.69 ⁰ 138.02 ⁰ 1.7859
142 ⁰ 1.6304 2.7239 257.7 2.19 253.97 ⁰ 183.98 ⁰ 2.3844 0.39 ⁰ 2.19 0.68 ⁰ 138.70 ⁰ 1.7999
143 ⁰ 1.6322 2.7471 259.9 2.20 256.13 ⁰ 184.37 ⁰ 2.3829 0.39 ⁰ 2.20 0.67 ⁰ 139.37 ⁰ 1.8138
144 ⁰ 1.6339 2.7704 262.1 2.20 258.30 ⁰ 184.75 ⁰ 2.3812 0.39 ⁰ 2.20 0.66 ⁰ 140.04 ⁰ 1.8276
145 ⁰ 1.6356 2.7937 264.3 2.21 260.48 ⁰ 185.14 ⁰ 2.3793 0.39 ⁰ 2.21 0.66 ⁰ 140.69 ⁰ 1.8412
146 ⁰ 1.6372 2.8171 266.5 2.21 262.66 ⁰ 185.53 ⁰ 2.3774 0.39 ⁰ 2.21 0.65 ⁰ 141.34 ⁰ 1.8546
147 ⁰ 1.6388 2.8405 268.7 2.21 264.84 ⁰ 185.93 ⁰ 2.3752 0.39 ⁰ 2.21 0.64 ⁰ 141.98 ⁰ 1.8678
148 ⁰ 1.6403 2.8639 270.9 2.22 267.03 ⁰ 186.32 ⁰ 2.3729 0.39 ⁰ 2.22 0.63 ⁰ 142.61 ⁰ 1.8809
149 ⁰ 1.6419 2.8874 273.2 2.22 269.22 ⁰ 186.72 ⁰ 2.3705 0.40 ⁰ 2.22 0.62 ⁰ 143.23 ⁰ 1.8938
150 ⁰ 1.6433 2.9110 275.4 2.23 271.41 ⁰ 187.11 ⁰ 2.3679 0.40 ⁰ 2.23 0.62 ⁰ 143.85 ⁰ 1.9066
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
151 ⁰ 1.6448 2.9346 277.6 2.23 273.61 ⁰ 187.51 ⁰ 2.3652 0.40 ⁰ 2.23 0.61 ⁰ 144.46 ⁰ 1.9193
152 ⁰ 1.6462 2.9582 279.8 2.24 275.82 ⁰ 187.91 ⁰ 2.3623 0.40 ⁰ 2.24 0.60 ⁰ 145.07 ⁰ 1.9317
153 ⁰ 1.6475 2.9819 282.1 2.24 278.02 ⁰ 188.31 ⁰ 2.3592 0.40 ⁰ 2.24 0.60 ⁰ 145.66 ⁰ 1.9440
154 ⁰ 1.6488 3.0056 284.3 2.24 280.23 ⁰ 188.72 ⁰ 2.3560 0.40 ⁰ 2.24 0.59 ⁰ 146.25 ⁰ 1.9561
155 ⁰ 1.6501 3.0293 286.6 2.25 282.45 ⁰ 189.12 ⁰ 2.3527 0.41 ⁰ 2.25 0.59 ⁰ 146.84 ⁰ 1.9681
156 ⁰ 1.6513 3.0531 288.8 2.25 284.66 ⁰ 189.53 ⁰ 2.3491 0.41 ⁰ 2.25 0.58 ⁰ 147.42 ⁰ 1.9799
157 ⁰ 1.6525 3.0769 291.1 2.25 286.88 ⁰ 189.94 ⁰ 2.3455 0.41 ⁰ 2.25 0.57 ⁰ 147.99 ⁰ 1.9915
158 ⁰ 1.6536 3.1007 293.3 2.26 289.11 ⁰ 190.35 ⁰ 2.3416 0.41 ⁰ 2.26 0.57 ⁰ 148.55 ⁰ 2.0029
159 ⁰ 1.6547 3.1246 295.6 2.26 291.33 ⁰ 190.76 ⁰ 2.3376 0.41 ⁰ 2.26 0.56 ⁰ 149.11 ⁰ 2.0142
160 ⁰ 1.6557 3.1485 297.9 2.26 293.56 ⁰ 191.18 ⁰ 2.3335 0.41 ⁰ 2.26 0.55 ⁰ 149.67 ⁰ 2.0253
161 ⁰ 1.6567 3.1725 300.1 2.26 295.79 ⁰ 191.59 ⁰ 2.3292 0.42 ⁰ 2.26 0.55 ⁰ 150.21 ⁰ 2.0363
162 ⁰ 1.6577 3.1964 302.4 2.27 298.03 ⁰ 192.01 ⁰ 2.3247 0.42 ⁰ 2.27 0.54 ⁰ 150.76 ⁰ 2.0470
163 ⁰ 1.6586 3.2204 304.7 2.27 300.27 ⁰ 192.43 ⁰ 2.3201 0.42 ⁰ 2.27 0.54 ⁰ 151.30 ⁰ 2.0577
164 ⁰ 1.6594 3.2445 306.9 2.27 302.51 ⁰ 192.85 ⁰ 2.3153 0.42 ⁰ 2.27 0.53 ⁰ 151.83 ⁰ 2.0681
165 ⁰ 1.6602 3.2685 309.2 2.27 304.75 ⁰ 193.28 ⁰ 2.3103 0.42 ⁰ 2.27 0.53 ⁰ 152.36 ⁰ 2.0784
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
166 ⁰ 1.6609 3.2926 311.5 2.28 306.99 ⁰ 193.71 ⁰ 2.3052 0.43 ⁰ 2.28 0.53 ⁰ 152.89 ⁰ 2.0885
167 ⁰ 1.6616 3.3166 313.8 2.28 309.24 ⁰ 194.14 ⁰ 2.2999 0.43 ⁰ 2.28 0.52 ⁰ 153.41 ⁰ 2.0984
168 ⁰ 1.6623 3.3407 316.0 2.28 311.48 ⁰ 194.57 ⁰ 2.2944 0.43 ⁰ 2.28 0.52 ⁰ 153.92 ⁰ 2.1082
169 ⁰ 1.6629 3.3649 318.3 2.28 313.73 ⁰ 195.01 ⁰ 2.2888 0.44 ⁰ 2.28 0.51 ⁰ 154.43 ⁰ 2.1178
170 ⁰ 1.6634 3.3890 320.6 2.28 315.98 ⁰ 195.44 ⁰ 2.2830 0.44 ⁰ 2.28 0.51 ⁰ 154.94 ⁰ 2.1272
171 ⁰ 1.6639 3.4132 322.9 2.28 318.24 ⁰ 195.88 ⁰ 2.2771 0.44 ⁰ 2.28 0.50 ⁰ 155.44 ⁰ 2.1364
172 ⁰ 1.6644 3.4373 325.2 2.29 320.49 ⁰ 196.32 ⁰ 2.2710 0.44 ⁰ 2.29 0.50 ⁰ 155.94 ⁰ 2.1455
173 ⁰ 1.6647 3.4615 327.5 2.29 322.74 ⁰ 196.77 ⁰ 2.2647 0.44 ⁰ 2.29 0.50 ⁰ 156.43 ⁰ 2.1544
174 ⁰ 1.6651 3.4857 329.7 2.29 325.00 ⁰ 197.22 ⁰ 2.2582 0.45 ⁰ 2.29 0.49 ⁰ 156.93 ⁰ 2.1632
175 ⁰ 1.6654 3.5099 332.0 2.29 327.25 ⁰ 197.67 ⁰ 2.2516 0.45 ⁰ 2.29 0.49 ⁰ 157.41 ⁰ 2.1718
176 ⁰ 1.6656 3.5341 334.3 2.29 329.51 ⁰ 198.12 ⁰ 2.2448 0.45 ⁰ 2.29 0.49 ⁰ 157.90 ⁰ 2.1802
177 ⁰ 1.6658 3.5583 336.6 2.29 331.77 ⁰ 198.58 ⁰ 2.2378 0.46 ⁰ 2.29 0.48 ⁰ 158.38 ⁰ 2.1884
178 ⁰ 1.6659 3.5825 338.9 2.29 334.03 ⁰ 199.04 ⁰ 2.2307 0.46 ⁰ 2.29 0.48 ⁰ 158.86 ⁰ 2.1965
179 ⁰ 1.6660 3.6068 341.2 2.29 336.29 ⁰ 199.50 ⁰ 2.2234 0.46 ⁰ 2.29 0.47 ⁰ 159.33 ⁰ 2.2044
180 ⁰ 1.6660 3.6310 343.5 2.29 338.54 ⁰ 199.96 ⁰ 2.2159 0.47 ⁰ 2.29 0.47 ⁰ 159.80 ⁰ 2.2121
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
181 ⁰ 1.6660 3.6552 345.8 2.29 340.80 ⁰ 200.43 ⁰ 2.2083 0.47 ⁰ 2.29 0.47 ⁰ 160.27 ⁰ 2.2196
182 ⁰ 1.6659 3.6794 348.1 2.29 343.06 ⁰ 200.90 ⁰ 2.2005 0.47 ⁰ 2.29 0.46 ⁰ 160.73 ⁰ 2.2270
183 ⁰ 1.6658 3.7036 350.4 2.29 345.32 ⁰ 201.38 ⁰ 2.1925 0.47 ⁰ 2.29 0.46 ⁰ 161.19 ⁰ 2.2342
184 ⁰ 1.6656 3.7278 352.7 2.29 347.58 ⁰ 201.86 ⁰ 2.1844 0.48 ⁰ 2.29 0.46 ⁰ 161.65 ⁰ 2.2413
185 ⁰ 1.6654 3.7521 354.9 2.29 349.83 ⁰ 202.34 ⁰ 2.1760 0.48 ⁰ 2.29 0.46 ⁰ 162.10 ⁰ 2.2482
186 ⁰ 1.6651 3.7762 357.2 2.29 352.09 ⁰ 202.83 ⁰ 2.1676 0.48 ⁰ 2.29 0.45 ⁰ 162.56 ⁰ 2.2549
187 ⁰ 1.6647 3.8004 359.5 2.29 354.34 ⁰ 203.32 ⁰ 2.1589 0.49 ⁰ 2.29 0.45 ⁰ 163.01 ⁰ 2.2614
188 ⁰ 1.6644 3.8246 361.8 2.29 356.60 ⁰ 203.81 ⁰ 2.1501 0.49 ⁰ 2.29 0.45 ⁰ 163.45 ⁰ 2.2678
189 ⁰ 1.6639 3.8488 364.1 2.29 358.85 ⁰ 204.31 ⁰ 2.1410 0.50 ⁰ 2.29 0.44 ⁰ 163.90 ⁰ 2.2740
190 ⁰ 1.6634 3.8729 366.4 2.28 1.10 ⁰ 204.81 ⁰ 2.1319 0.50 ⁰ 2.28 0.44 ⁰ 164.34 ⁰ 2.2800
191 ⁰ 1.6629 3.8971 368.7 2.28 3.36 ⁰ 205.31 ⁰ 2.1226 0.50 ⁰ 2.28 0.44 ⁰ 164.77 ⁰ 2.2859
192 ⁰ 1.6623 3.9212 370.9 2.28 5.60 ⁰ 205.82 ⁰ 2.1131 0.51 ⁰ 2.28 0.44 ⁰ 165.21 ⁰ 2.2916
193 ⁰ 1.6616 3.9453 373.2 2.28 7.85 ⁰ 206.33 ⁰ 2.1034 0.51 ⁰ 2.28 0.43 ⁰ 165.64 ⁰ 2.2971
194 ⁰ 1.6609 3.9694 375.5 2.28 10.10 ⁰ 206.85 ⁰ 2.0935 0.52 ⁰ 2.28 0.43 ⁰ 166.08 ⁰ 2.3025
195 ⁰ 1.6602 3.9935 377.8 2.28 12.34 ⁰ 207.38 ⁰ 2.0835 0.52 ⁰ 2.28 0.43 ⁰ 166.51 ⁰ 2.3078
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
196 ⁰ 1.6594 4.0175 380.1 2.27 14.58 ⁰ 207.90 ⁰ 2.0733 0.53 ⁰ 2.27 0.43 ⁰ 166.93 ⁰ 2.3128
197 ⁰ 1.6586 4.0415 382.3 2.27 16.82 ⁰ 208.43 ⁰ 2.0630 0.53 ⁰ 2.27 0.42 ⁰ 167.35 ⁰ 2.3177
198 ⁰ 1.6577 4.0655 384.6 2.27 19.06 ⁰ 208.97 ⁰ 2.0525 0.54 ⁰ 2.27 0.42 ⁰ 167.78 ⁰ 2.3224
199 ⁰ 1.6567 4.0895 386.9 2.27 21.29 ⁰ 209.51 ⁰ 2.0417 0.54 ⁰ 2.27 0.42 ⁰ 168.20 ⁰ 2.3269
200 ⁰ 1.6557 4.1134 389.1 2.26 23.53 ⁰ 210.06 ⁰ 2.0309 0.55 ⁰ 2.26 0.42 ⁰ 168.61 ⁰ 2.3313
201 ⁰ 1.6547 4.1373 391.4 2.26 25.75 ⁰ 210.61 ⁰ 2.0199 0.55 ⁰ 2.26 0.42 ⁰ 169.03 ⁰ 2.3355
202 ⁰ 1.6536 4.1612 393.6 2.26 27.98 ⁰ 211.17 ⁰ 2.0087 0.56 ⁰ 2.26 0.41 ⁰ 169.44 ⁰ 2.3396
203 ⁰ 1.6525 4.1850 395.9 2.26 30.20 ⁰ 211.73 ⁰ 1.9973 0.56 ⁰ 2.26 0.41 ⁰ 169.85 ⁰ 2.3435
204 ⁰ 1.6513 4.2089 398.2 2.25 32.42 ⁰ 212.30 ⁰ 1.9857 0.57 ⁰ 2.25 0.41 ⁰ 170.26 ⁰ 2.3473
205 ⁰ 1.6501 4.2326 400.4 2.25 34.64 ⁰ 212.87 ⁰ 1.9740 0.57 ⁰ 2.25 0.41 ⁰ 170.67 ⁰ 2.3509
206 ⁰ 1.6488 4.2564 402.7 2.25 36.86 ⁰ 213.46 ⁰ 1.9621 0.58 ⁰ 2.25 0.41 ⁰ 171.08 ⁰ 2.3543
207 ⁰ 1.6475 4.2801 404.9 2.24 39.07 ⁰ 214.04 ⁰ 1.9501 0.59 ⁰ 2.24 0.40 ⁰ 171.48 ⁰ 2.3576
208 ⁰ 1.6462 4.3038 407.1 2.24 41.27 ⁰ 214.63 ⁰ 1.9379 0.59 ⁰ 2.24 0.40 ⁰ 171.88 ⁰ 2.3607
209 ⁰ 1.6448 4.3274 409.4 2.24 43.48 ⁰ 215.23 ⁰ 1.9256 0.60 ⁰ 2.24 0.40 ⁰ 172.29 ⁰ 2.3637
210 ⁰ 1.6433 4.3510 411.6 2.23 45.67 ⁰ 215.84 ⁰ 1.9131 0.61 ⁰ 2.23 0.40 ⁰ 172.68 ⁰ 2.3665
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
211 ⁰ 1.6419 4.3745 413.8 2.23 47.87 ⁰ 216.45 ⁰ 1.9003 0.61 ⁰ 2.23 0.40 ⁰ 173.08 ⁰ 2.3692
212 ⁰ 1.6403 4.3980 416.1 2.22 50.06 ⁰ 217.07 ⁰ 1.8875 0.62 ⁰ 2.22 0.40 ⁰ 173.48 ⁰ 2.3717
213 ⁰ 1.6388 4.4215 418.3 2.22 52.25 ⁰ 217.70 ⁰ 1.8745 0.63 ⁰ 2.22 0.40 ⁰ 173.87 ⁰ 2.3741
214 ⁰ 1.6372 4.4449 420.5 2.21 54.43 ⁰ 218.33 ⁰ 1.8614 0.63 ⁰ 2.21 0.39 ⁰ 174.26 ⁰ 2.3763
215 ⁰ 1.6356 4.4683 422.7 2.21 56.61 ⁰ 218.97 ⁰ 1.8481 0.64 ⁰ 2.21 0.39 ⁰ 174.66 ⁰ 2.3783
216 ⁰ 1.6339 4.4916 424.9 2.21 58.78 ⁰ 219.63 ⁰ 1.8346 0.65 ⁰ 2.21 0.39 ⁰ 175.05 ⁰ 2.3803
217 ⁰ 1.6322 4.5148 427.1 2.20 60.95 ⁰ 220.28 ⁰ 1.8210 0.66 ⁰ 2.20 0.39 ⁰ 175.43 ⁰ 2.3820
218 ⁰ 1.6304 4.5381 429.3 2.20 63.12 ⁰ 220.95 ⁰ 1.8071 0.67 ⁰ 2.20 0.39 ⁰ 175.82 ⁰ 2.3836
219 ⁰ 1.6286 4.5612 431.5 2.19 65.28 ⁰ 221.63 ⁰ 1.7932 0.68 ⁰ 2.19 0.38 ⁰ 176.21 ⁰ 2.3851
220 ⁰ 1.6268 4.5844 433.7 2.19 67.44 ⁰ 222.32 ⁰ 1.7791 0.69 ⁰ 2.19 0.39 ⁰ 176.59 ⁰ 2.3864
221 ⁰ 1.6250 4.6074 435.9 2.18 69.59 ⁰ 223.01 ⁰ 1.7648 0.70 ⁰ 2.18 0.38 ⁰ 176.98 ⁰ 2.3876
222 ⁰ 1.6231 4.6304 438.0 2.18 71.73 ⁰ 223.72 ⁰ 1.7503 0.71 ⁰ 2.18 0.38 ⁰ 177.36 ⁰ 2.3887
223 ⁰ 1.6212 4.6534 440.2 2.17 73.87 ⁰ 224.43 ⁰ 1.7357 0.72 ⁰ 2.17 0.38 ⁰ 177.74 ⁰ 2.3896
224 ⁰ 1.6192 4.6763 442.4 2.17 76.01 ⁰ 225.16 ⁰ 1.7210 0.73 ⁰ 2.17 0.38 ⁰ 178.12 ⁰ 2.3903
225 ⁰ 1.6172 4.6992 444.5 2.16 78.14 ⁰ 225.90 ⁰ 1.7061 0.74 ⁰ 2.16 0.38 ⁰ 178.50 ⁰ 2.3909
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
226 ⁰ 1.6152 4.7220 446.7 2.16 80.27 ⁰ 226.64 ⁰ 1.6911 0.75 ⁰ 2.16 0.38 ⁰ 178.88 ⁰ 2.3914
227 ⁰ 1.6132 4.7447 448.8 2.15 82.39 ⁰ 227.40 ⁰ 1.6759 0.76 ⁰ 2.15 0.38 ⁰ 179.25 ⁰ 2.3917
228 ⁰ 1.6111 4.7674 451.0 2.15 84.50 ⁰ 228.18 ⁰ 1.6605 0.77 ⁰ 2.15 0.38 ⁰ 179.63 ⁰ 2.3919
229 ⁰ 1.6090 4.7900 453.1 2.14 86.61 ⁰ 228.96 ⁰ 1.6450 0.78 ⁰ 2.14 0.38 ⁰ 180.01 ⁰ 2.3920
230 ⁰ 1.6069 4.8126 455.3 2.13 88.71 ⁰ 229.76 ⁰ 1.6294 0.80 ⁰ 2.13 0.38 ⁰ 180.38 ⁰ 2.3919
231 ⁰ 1.6047 4.8351 457.4 2.13 90.81 ⁰ 231.00 ⁰ 1.6052 0.81 ⁰ 2.13 0.37 ⁰ 180.75 ⁰ 2.3917
232 ⁰ 1.6026 4.8575 459.5 2.12 92.90 ⁰ 231.83 ⁰ 1.5892 0.83 ⁰ 2.12 0.37 ⁰ 181.12 ⁰ 2.3914
233 ⁰ 1.6004 4.8799 461.6 2.12 94.99 ⁰ 232.68 ⁰ 1.5730 0.85 ⁰ 2.12 0.37 ⁰ 181.50 ⁰ 2.3909
234 ⁰ 1.5982 4.9022 463.8 2.11 97.07 ⁰ 233.54 ⁰ 1.5567 0.86 ⁰ 2.11 0.37 ⁰ 181.87 ⁰ 2.3903
235 ⁰ 1.5959 4.9245 465.9 2.11 99.15 ⁰ 234.43 ⁰ 1.5402 0.88 ⁰ 2.11 0.37 ⁰ 182.24 ⁰ 2.3896
236 ⁰ 1.5937 4.9467 468.0 2.10 101.22 ⁰ 235.32 ⁰ 1.5236 0.90 ⁰ 2.10 0.37 ⁰ 182.61 ⁰ 2.3887
237 ⁰ 1.5914 4.9688 470.0 2.09 103.28 ⁰ 236.23 ⁰ 1.5069 0.91 ⁰ 2.09 0.37 ⁰ 182.98 ⁰ 2.3878
238 ⁰ 1.5891 4.9909 472.1 2.09 105.34 ⁰ 237.17 ⁰ 1.4900 0.93 ⁰ 2.09 0.37 ⁰ 183.34 ⁰ 2.3866
239 ⁰ 1.5867 5.0129 474.2 2.08 107.39 ⁰ 238.12 ⁰ 1.4730 0.95 ⁰ 2.08 0.37 ⁰ 183.71 ⁰ 2.3854
240 ⁰ 1.5844 5.0348 476.3 2.08 109.43 ⁰ 239.08 ⁰ 1.4559 0.97 ⁰ 2.08 0.37 ⁰ 184.08 ⁰ 2.3840
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
241 ⁰ 1.5821 5.0567 478.4 2.07 111.47 ⁰ 240.08 ⁰ 1.4387 0.99 ⁰ 2.07 0.37 ⁰ 184.44 ⁰ 2.3826
242 ⁰ 1.5797 5.0785 480.4 2.06 113.51 ⁰ 241.09 ⁰ 1.4213 1.01 ⁰ 2.06 0.36 ⁰ 184.80 ⁰ 2.3810
243 ⁰ 1.5773 5.1002 482.5 2.06 115.54 ⁰ 242.12 ⁰ 1.4038 1.04 ⁰ 2.06 0.36 ⁰ 185.17 ⁰ 2.3792
244 ⁰ 1.5749 5.1219 484.5 2.05 117.56 ⁰ 243.17 ⁰ 1.3862 1.05 ⁰ 2.05 0.36 ⁰ 185.53 ⁰ 2.3774
245 ⁰ 1.5725 5.1435 486.6 2.04 119.57 ⁰ 244.25 ⁰ 1.3686 1.08 ⁰ 2.04 0.36 ⁰ 185.89 ⁰ 2.3754
246 ⁰ 1.5701 5.1651 488.6 2.04 121.58 ⁰ 245.35 ⁰ 1.3508 1.10 ⁰ 2.04 0.36 ⁰ 186.25 ⁰ 2.3733
247 ⁰ 1.5676 5.1866 490.6 2.03 123.58 ⁰ 246.48 ⁰ 1.3329 1.13 ⁰ 2.03 0.36 ⁰ 186.62 ⁰ 2.3711
248 ⁰ 1.5652 5.2080 492.7 2.03 125.58 ⁰ 247.63 ⁰ 1.3149 1.16 ⁰ 2.03 0.36 ⁰ 186.98 ⁰ 2.3688
249 ⁰ 1.5627 5.2293 494.7 2.02 127.57 ⁰ 248.82 ⁰ 1.2968 1.18 ⁰ 2.02 0.36 ⁰ 187.34 ⁰ 2.3664
250 ⁰ 1.5603 5.2506 496.7 2.01 129.55 ⁰ 250.03 ⁰ 1.2787 1.21 ⁰ 2.01 0.36 ⁰ 187.70 ⁰ 2.3639
251 ⁰ 1.5578 5.2718 498.7 2.01 131.53 ⁰ 251.28 ⁰ 1.2604 1.25 ⁰ 2.01 0.36 ⁰ 188.06 ⁰ 2.3612
252 ⁰ 1.5553 5.2929 500.7 2.00 133.50 ⁰ 252.56 ⁰ 1.2420 1.28 ⁰ 2.00 0.36 ⁰ 188.42 ⁰ 2.3584
253 ⁰ 1.5528 5.3140 502.7 1.99 135.47 ⁰ 253.87 ⁰ 1.2236 1.31 ⁰ 1.99 0.36 ⁰ 188.78 ⁰ 2.3556
254 ⁰ 1.5503 5.3350 504.7 1.99 137.43 ⁰ 255.21 ⁰ 1.2051 1.35 ⁰ 1.99 0.36 ⁰ 189.13 ⁰ 2.3526
255 ⁰ 1.5478 5.3560 506.7 1.98 139.38 ⁰ 256.60 ⁰ 1.1866 1.39 ⁰ 1.98 0.36 ⁰ 189.49 ⁰ 2.3495
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
256 ⁰ 1.5453 5.3768 508.6 1.97 141.32 ⁰ 258.02 ⁰ 1.1681 1.42 ⁰ 1.97 0.36 ⁰ 189.85 ⁰ 2.3463
257 ⁰ 1.5428 5.3976 510.6 1.97 143.26 ⁰ 259.49 ⁰ 1.1494 1.47 ⁰ 1.97 0.36 ⁰ 190.21 ⁰ 2.3430
258 ⁰ 1.5403 5.4184 512.6 1.96 145.20 ⁰ 261.00 ⁰ 1.1308 1.51 ⁰ 1.96 0.36 ⁰ 190.57 ⁰ 2.3395
259 ⁰ 1.5378 5.4391 514.5 1.96 147.13 ⁰ 262.56 ⁰ 1.1120 1.56 ⁰ 1.96 0.36 ⁰ 190.93 ⁰ 2.3360
260 ⁰ 1.5353 5.4597 516.5 1.95 149.05 ⁰ 264.16 ⁰ 1.0933 1.61 ⁰ 1.95 0.36 ⁰ 191.28 ⁰ 2.3324
261 ⁰ 1.5328 5.4802 518.4 1.94 150.96 ⁰ 265.81 ⁰ 1.0747 1.65 ⁰ 1.94 0.36 ⁰ 191.64 ⁰ 2.3287
262 ⁰ 1.5303 5.5007 520.4 1.94 152.87 ⁰ 267.52 ⁰ 1.0560 1.71 ⁰ 1.94 0.36 ⁰ 192.00 ⁰ 2.3248
263 ⁰ 1.5278 5.5211 522.3 1.93 154.77 ⁰ 269.29 ⁰ 1.0373 1.77 ⁰ 1.93 0.36 ⁰ 192.36 ⁰ 2.3209
264 ⁰ 1.5253 5.5414 524.2 1.92 156.67 ⁰ 271.11 ⁰ 1.0188 1.82 ⁰ 1.92 0.36 ⁰ 192.72 ⁰ 2.3169
265 ⁰ 1.5228 5.5617 526.1 1.92 158.56 ⁰ 272.99 ⁰ 1.0003 1.88 ⁰ 1.92 0.36 ⁰ 193.07 ⁰ 2.3127
266 ⁰ 1.5203 5.5819 528.0 1.91 160.44 ⁰ 274.94 ⁰ 0.9819 1.94 ⁰ 1.91 0.36 ⁰ 193.43 ⁰ 2.3085
267 ⁰ 1.5178 5.6020 530.0 1.91 162.32 ⁰ 276.96 ⁰ 0.9636 2.02 ⁰ 1.91 0.36 ⁰ 193.79 ⁰ 2.3042
268 ⁰ 1.5154 5.6221 531.9 1.90 164.19 ⁰ 279.04 ⁰ 0.9454 2.09 ⁰ 1.90 0.36 ⁰ 194.15 ⁰ 2.2998
269 ⁰ 1.5129 5.6421 533.7 1.89 166.06 ⁰ 281.20 ⁰ 0.9274 2.16 ⁰ 1.89 0.36 ⁰ 194.51 ⁰ 2.2952
270 ⁰ 1.5104 5.6620 535.6 1.89 167.92 ⁰ 283.44 ⁰ 0.9096 2.24 ⁰ 1.89 0.36 ⁰ 194.87 ⁰ 2.2906
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
271 ⁰ 1.5080 5.6819 537.5 1.88 169.77 ⁰ 285.64 ⁰ 0.8929 2.20 ⁰ 1.88 0.36 ⁰ 195.23 ⁰ 2.2859
272 ⁰ 1.5055 5.7017 539.4 1.87 171.62 ⁰ 287.93 ⁰ 0.8764 2.29 ⁰ 1.87 0.36 ⁰ 195.59 ⁰ 2.2811
273 ⁰ 1.5031 5.7215 541.3 1.87 173.46 ⁰ 290.30 ⁰ 0.8601 2.37 ⁰ 1.87 0.36 ⁰ 195.95 ⁰ 2.2762
274 ⁰ 1.5006 5.7412 543.1 1.86 175.29 ⁰ 292.75 ⁰ 0.8441 2.45 ⁰ 1.86 0.36 ⁰ 196.31 ⁰ 2.2712
275 ⁰ 1.4982 5.7608 545.0 1.86 177.12 ⁰ 295.28 ⁰ 0.8286 2.53 ⁰ 1.86 0.36 ⁰ 196.67 ⁰ 2.2661
276 ⁰ 1.4958 5.7803 546.8 1.85 178.95 ⁰ 297.90 ⁰ 0.8133 2.62 ⁰ 1.85 0.36 ⁰ 197.03 ⁰ 2.2609
277 ⁰ 1.4934 5.7998 548.7 1.84 180.76 ⁰ 300.62 ⁰ 0.7984 2.72 ⁰ 1.84 0.36 ⁰ 197.39 ⁰ 2.2557
278 ⁰ 1.4910 5.8193 550.5 1.84 182.58 ⁰ 303.44 ⁰ 0.7840 2.82 ⁰ 1.84 0.36 ⁰ 197.75 ⁰ 2.2503
279 ⁰ 1.4887 5.8386 552.3 1.83 184.38 ⁰ 306.34 ⁰ 0.7701 2.90 ⁰ 1.83 0.36 ⁰ 198.12 ⁰ 2.2449
280 ⁰ 1.4863 5.8579 554.2 1.83 186.18 ⁰ 309.35 ⁰ 0.7568 3.01 ⁰ 1.83 0.36 ⁰ 198.48 ⁰ 2.2393
281 ⁰ 1.4840 5.8772 556.0 1.82 187.98 ⁰ 312.44 ⁰ 0.7441 3.09 ⁰ 1.82 0.37 ⁰ 198.85 ⁰ 2.2337
282 ⁰ 1.4816 5.8964 557.8 1.82 189.77 ⁰ 315.63 ⁰ 0.7320 3.19 ⁰ 1.82 0.37 ⁰ 199.21 ⁰ 2.2280
283 ⁰ 1.4793 5.9155 559.6 1.81 191.55 ⁰ 318.91 ⁰ 0.7207 3.28 ⁰ 1.81 0.36 ⁰ 199.58 ⁰ 2.2222
284 ⁰ 1.4770 5.9346 561.4 1.80 193.33 ⁰ 322.30 ⁰ 0.7101 3.39 ⁰ 1.80 0.37 ⁰ 199.94 ⁰ 2.2163
285 ⁰ 1.4748 5.9536 563.2 1.80 195.10 ⁰ 325.77 ⁰ 0.7003 3.47 ⁰ 1.80 0.37 ⁰ 200.31 ⁰ 2.2103
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
286 ⁰ 1.4725 5.9725 565.0 1.79 196.87 ⁰ 329.47 ⁰ 0.6911 3.70 ⁰ 1.79 0.37 ⁰ 200.68 ⁰ 2.2043
287 ⁰ 1.4703 5.9914 566.8 1.79 198.63 ⁰ 333.26 ⁰ 0.6828 3.79 ⁰ 1.79 0.37 ⁰ 201.05 ⁰ 2.1981
288 ⁰ 1.4680 6.0103 568.6 1.78 200.38 ⁰ 337.12 ⁰ 0.6756 3.87 ⁰ 1.78 0.37 ⁰ 201.42 ⁰ 2.1919
289 ⁰ 1.4658 6.0290 570.3 1.78 202.13 ⁰ 341.05 ⁰ 0.6695 3.93 ⁰ 1.78 0.37 ⁰ 201.79 ⁰ 2.1855
290 ⁰ 1.4637 6.0478 572.1 1.77 203.88 ⁰ 345.03 ⁰ 0.6645 3.98 ⁰ 1.77 0.37 ⁰ 202.16 ⁰ 2.1791
291 ⁰ 1.4615 6.0664 573.9 1.77 205.62 ⁰ 349.06 ⁰ 0.6607 4.03 ⁰ 1.77 0.37 ⁰ 202.54 ⁰ 2.1726
292 ⁰ 1.4594 6.0850 575.6 1.76 207.36 ⁰ 353.11 ⁰ 0.6580 4.06 ⁰ 1.76 0.37 ⁰ 202.91 ⁰ 2.1661
293 ⁰ 1.4572 6.1036 577.4 1.76 209.09 ⁰ 357.19 ⁰ 0.6566 4.08 ⁰ 1.76 0.38 ⁰ 203.29 ⁰ 2.1594
294 ⁰ 1.4551 6.1221 579.2 1.75 210.81 ⁰ 1.26 ⁰ 0.6564 4.07 ⁰ 1.75 0.38 ⁰ 203.66 ⁰ 2.1527
295 ⁰ 1.4531 6.1406 580.9 1.75 212.53 ⁰ 5.33 ⁰ 0.6573 4.07 ⁰ 1.75 0.38 ⁰ 204.04 ⁰ 2.1459
296 ⁰ 1.4510 6.1590 582.6 1.74 214.25 ⁰ 9.35 ⁰ 0.6595 4.02 ⁰ 1.74 0.38 ⁰ 204.42 ⁰ 2.1390
297 ⁰ 1.4490 6.1773 584.4 1.74 215.96 ⁰ 13.33 ⁰ 0.6628 3.98 ⁰ 1.74 0.38 ⁰ 204.80 ⁰ 2.1320
298 ⁰ 1.4470 6.1956 586.1 1.73 217.66 ⁰ 17.25 ⁰ 0.6672 3.92 ⁰ 1.73 0.38 ⁰ 205.19 ⁰ 2.1249
299 ⁰ 1.4450 6.2138 587.8 1.73 219.37 ⁰ 21.11 ⁰ 0.6727 3.86 ⁰ 1.73 0.38 ⁰ 205.57 ⁰ 2.1178
300 ⁰ 1.4430 6.2320 589.6 1.72 221.06 ⁰ 24.88 ⁰ 0.6792 3.77 ⁰ 1.72 0.38 ⁰ 205.95 ⁰ 2.1106
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
301 ⁰ 1.4411 6.2502 591.3 1.72 222.75 ⁰ 28.58 ⁰ 0.6867 3.70 ⁰ 1.72 0.39 ⁰ 206.34 ⁰ 2.1032
302 ⁰ 1.4392 6.2683 593.0 1.71 224.44 ⁰ 32.17 ⁰ 0.6950 3.59 ⁰ 1.71 0.39 ⁰ 206.73 ⁰ 2.0958
303 ⁰ 1.4373 6.2863 594.7 1.71 226.12 ⁰ 35.66 ⁰ 0.7042 3.49 ⁰ 1.71 0.39 ⁰ 207.12 ⁰ 2.0884
304 ⁰ 1.4355 6.3043 596.4 1.70 227.80 ⁰ 39.05 ⁰ 0.7142 3.39 ⁰ 1.70 0.39 ⁰ 207.51 ⁰ 2.0808
305 ⁰ 1.4336 6.3223 598.1 1.70 229.48 ⁰ 42.33 ⁰ 0.7249 3.28 ⁰ 1.70 0.39 ⁰ 207.91 ⁰ 2.0732
306 ⁰ 1.4318 6.3402 599.8 1.69 231.15 ⁰ 45.50 ⁰ 0.7362 3.17 ⁰ 1.69 0.39 ⁰ 208.30 ⁰ 2.0656
307 ⁰ 1.4300 6.3581 601.5 1.69 232.81 ⁰ 48.57 ⁰ 0.7481 3.07 ⁰ 1.69 0.40 ⁰ 208.70 ⁰ 2.0577
308 ⁰ 1.4283 6.3759 603.2 1.69 234.48 ⁰ 51.55 ⁰ 0.7607 2.98 ⁰ 1.69 0.40 ⁰ 209.10 ⁰ 2.0499
309 ⁰ 1.4266 6.3937 604.8 1.68 236.13 ⁰ 54.40 ⁰ 0.7736 2.85 ⁰ 1.68 0.40 ⁰ 209.50 ⁰ 2.0419
310 ⁰ 1.4249 6.4114 606.5 1.68 237.79 ⁰ 57.16 ⁰ 0.7870 2.76 ⁰ 1.68 0.40 ⁰ 209.91 ⁰ 2.0339
311 ⁰ 1.4232 6.4291 608.2 1.67 239.44 ⁰ 59.80 ⁰ 0.8007 2.65 ⁰ 1.67 0.41 ⁰ 210.31 ⁰ 2.0258
312 ⁰ 1.4216 6.4468 609.9 1.67 241.08 ⁰ 62.36 ⁰ 0.8147 2.56 ⁰ 1.67 0.41 ⁰ 210.72 ⁰ 2.0176
313 ⁰ 1.4200 6.4644 611.5 1.67 242.73 ⁰ 64.83 ⁰ 0.8292 2.48 ⁰ 1.67 0.41 ⁰ 211.13 ⁰ 2.0094
314 ⁰ 1.4184 6.4820 613.2 1.66 244.37 ⁰ 67.21 ⁰ 0.8439 2.38 ⁰ 1.66 0.41 ⁰ 211.54 ⁰ 2.0010
315 ⁰ 1.4168 6.4995 614.9 1.66 246.00 ⁰ 69.50 ⁰ 0.8588 2.29 ⁰ 1.66 0.42 ⁰ 211.96 ⁰ 1.9926
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
316 ⁰ 1.4153 6.5170 616.5 1.66 247.63 ⁰ 71.71 ⁰ 0.8738 2.21 ⁰ 1.66 0.42 ⁰ 212.38 ⁰ 1.9841
317 ⁰ 1.4138 6.5345 618.2 1.65 249.26 ⁰ 73.84 ⁰ 0.8891 2.13 ⁰ 1.65 0.42 ⁰ 212.80 ⁰ 1.9755
318 ⁰ 1.4124 6.5519 619.8 1.65 250.88 ⁰ 75.89 ⁰ 0.9045 2.05 ⁰ 1.65 0.43 ⁰ 213.23 ⁰ 1.9668
319 ⁰ 1.4110 6.5693 621.5 1.65 252.51 ⁰ 77.87 ⁰ 0.9199 1.98 ⁰ 1.65 0.43 ⁰ 213.66 ⁰ 1.9580
320 ⁰ 1.4096 6.5866 623.1 1.64 254.12 ⁰ 79.78 ⁰ 0.9355 1.91 ⁰ 1.64 0.43 ⁰ 214.09 ⁰ 1.9492
321 ⁰ 1.4082 6.6040 624.7 1.64 255.74 ⁰ 81.62 ⁰ 0.9511 1.84 ⁰ 1.64 0.43 ⁰ 214.52 ⁰ 1.9403
322 ⁰ 1.4069 6.6213 626.4 1.64 257.35 ⁰ 83.40 ⁰ 0.9667 1.78 ⁰ 1.64 0.44 ⁰ 214.96 ⁰ 1.9313
323 ⁰ 1.4056 6.6385 628.0 1.63 258.96 ⁰ 85.12 ⁰ 0.9824 1.72 ⁰ 1.63 0.44 ⁰ 215.40 ⁰ 1.9222
324 ⁰ 1.4043 6.6557 629.6 1.63 260.57 ⁰ 86.78 ⁰ 0.9981 1.66 ⁰ 1.63 0.44 ⁰ 215.84 ⁰ 1.9130
325 ⁰ 1.4031 6.6729 631.3 1.63 262.17 ⁰ 88.39 ⁰ 1.0138 1.61 ⁰ 1.63 0.45 ⁰ 216.29 ⁰ 1.9038
326 ⁰ 1.4019 6.6901 632.9 1.62 263.77 ⁰ 89.94 ⁰ 1.0294 1.55 ⁰ 1.62 0.45 ⁰ 216.74 ⁰ 1.8945
327 ⁰ 1.4007 6.7072 634.5 1.62 265.37 ⁰ 91.45 ⁰ 1.0450 1.51 ⁰ 1.62 0.45 ⁰ 217.19 ⁰ 1.8851
328 ⁰ 1.3996 6.7243 636.1 1.62 266.96 ⁰ 92.91 ⁰ 1.0607 1.47 ⁰ 1.62 0.46 ⁰ 217.65 ⁰ 1.8756
329 ⁰ 1.3985 6.7414 637.7 1.62 268.56 ⁰ 94.33 ⁰ 1.0762 1.42 ⁰ 1.62 0.46 ⁰ 218.11 ⁰ 1.8660
330 ⁰ 1.3974 6.7585 639.4 1.61 270.15 ⁰ 95.70 ⁰ 1.0917 1.37 ⁰ 1.61 0.47 ⁰ 218.58 ⁰ 1.8563
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
331 ⁰ 1.3964 6.7755 641.0 1.61 271.73 ⁰ 97.03 ⁰ 1.1072 1.33 ⁰ 1.61 0.47 ⁰ 219.05 ⁰ 1.8466
332 ⁰ 1.3954 6.7925 642.6 1.61 273.32 ⁰ 98.33 ⁰ 1.1226 1.30 ⁰ 1.61 0.47 ⁰ 219.52 ⁰ 1.8367
333 ⁰ 1.3944 6.8095 644.2 1.61 274.90 ⁰ 99.59 ⁰ 1.1379 1.26 ⁰ 1.61 0.48 ⁰ 220.00 ⁰ 1.8268
334 ⁰ 1.3934 6.8264 645.8 1.60 276.48 ⁰ 100.813 ⁰ 1.1532 1.22 ⁰ 1.60 0.48 ⁰ 220.48 ⁰ 1.8168
335 ⁰ 1.3925 6.8434 647.4 1.60 278.06 ⁰ 102.00 ⁰ 1.1683 1.19 ⁰ 1.60 0.49 ⁰ 220.97 ⁰ 1.8067
336 ⁰ 1.3917 6.8603 649.0 1.60 279.64 ⁰ 103.16 ⁰ 1.1834 1.16 ⁰ 1.60 0.49 ⁰ 221.47 ⁰ 1.7966
337 ⁰ 1.3908 6.8772 650.6 1.60 281.21 ⁰ 104.29 ⁰ 1.1984 1.13 ⁰ 1.60 0.50 ⁰ 221.97 ⁰ 1.7862
338 ⁰ 1.3900 6.8940 652.2 1.60 282.79 ⁰ 105.39 ⁰ 1.2133 1.10 ⁰ 1.60 0.50 ⁰ 222.47 ⁰ 1.7759
339 ⁰ 1.3893 6.9109 653.8 1.59 284.36 ⁰ 106.46 ⁰ 1.2281 1.07 ⁰ 1.59 0.51 ⁰ 222.98 ⁰ 1.7654
340 ⁰ 1.3886 6.9277 655.4 1.59 285.93 ⁰ 107.50 ⁰ 1.2428 1.04 ⁰ 1.59 0.51 ⁰ 223.49 ⁰ 1.7549
341 ⁰ 1.3879 6.9446 657.0 1.59 287.50 ⁰ 108.52 ⁰ 1.2573 1.02 ⁰ 1.59 0.52 ⁰ 224.01 ⁰ 1.7443
342 ⁰ 1.3872 6.9614 658.5 1.59 289.06 ⁰ 109.51 ⁰ 1.2719 1.00 ⁰ 1.59 0.53 ⁰ 224.54 ⁰ 1.7336
343 ⁰ 1.3866 6.9781 660.1 1.59 290.63 ⁰ 110.49 ⁰ 1.2863 0.97 ⁰ 1.59 0.53 ⁰ 225.07 ⁰ 1.7227
344 ⁰ 1.3860 6.9949 661.7 1.59 292.19 ⁰ 111.44 ⁰ 1.3006 0.95 ⁰ 1.59 0.54 ⁰ 225.61 ⁰ 1.7118
345 ⁰ 1.3854 7.0117 663.3 1.59 293.75 ⁰ 112.37 ⁰ 1.3149 0.93 ⁰ 1.59 0.55 ⁰ 226.16 ⁰ 1.7008
θ R(AU) A(AU)2 T (dy) Δt(dy) θ θC1 RC1(AU) ∆θC1 ΔtCy(dy) ∆θC2 θC2 RC2(AU)
346 ⁰ 1.3849 7.0284 664.9 1.58 295.31 ⁰ 113.27 ⁰ 1.3289 0.90 ⁰ 1.58 0.55 ⁰ 226.71 ⁰ 1.6898
347 ⁰ 1.3844 7.0451 666.5 1.58 296.87 ⁰ 114.155 ⁰ 1.3429 0.89 ⁰ 1.58 0.56 ⁰ 227.27 ⁰ 1.6786
348 ⁰ 1.3840 7.0619 668.1 1.58 298.43 ⁰ 115.025 ⁰ 1.3568 0.87 ⁰ 1.58 0.56 ⁰ 227.83 ⁰ 1.6673
349 ⁰ 1.3836 7.0786 669.6 1.58 299.99 ⁰ 115.875 ⁰ 1.3706 0.85 ⁰ 1.58 0.57 ⁰ 228.40 ⁰ 1.6560
350 ⁰ 1.3832 7.0953 671.2 1.58 301.55 ⁰ 116.71 ⁰ 1.3843 0.83 ⁰ 1.58 0.58 ⁰ 228.98 ⁰ 1.6445
351 ⁰ 1.3829 7.1120 672.8 1.58 303.10 ⁰ 117.53 ⁰ 1.3978 0.82 ⁰ 1.58 0.59 ⁰ 229.57 ⁰ 1.6330
352 ⁰ 1.3825 7.1286 674.4 1.58 304.66 ⁰ 118.33 ⁰ 1.4113 0.80 ⁰ 1.58 0.60 ⁰ 230.17 ⁰ 1.6213
353 ⁰ 1.3823 7.1453 675.9 1.58 306.21 ⁰ 119.12 ⁰ 1.4247 0.79 ⁰ 1.58 0.61 ⁰ 230.78 ⁰ 1.6095
354 ⁰ 1.3820 7.1620 677.5 1.58 307.77 ⁰ 119.89 ⁰ 1.4380 0.77 ⁰ 1.58 0.61 ⁰ 231.39 ⁰ 1.5977
355 ⁰ 1.3818 7.1787 679.1 1.58 309.32 ⁰ 120.64 ⁰ 1.4512 0.76 ⁰ 1.58 0.62 ⁰ 232.02 ⁰ 1.5857
356 ⁰ 1.3817 7.1953 680.7 1.58 310.88 ⁰ 121.39 ⁰ 1.4642 0.74 ⁰ 1.58 0.63 ⁰ 232.65 ⁰ 1.5736
357 ⁰ 1.3816 7.2120 682.3 1.58 312.43 ⁰ 122.12 ⁰ 1.4772 0.73 ⁰ 1.58 0.64 ⁰ 233.29 ⁰ 1.5615
358 ⁰ 1.3815 7.2286 683.8 1.58 313.98 ⁰ 122.84 ⁰ 1.4901 0.72 ⁰ 1.58 0.65 ⁰ 233.94 ⁰ 1.5492
359 ⁰ 1.3814 7.2453 685.4 1.58 315.54 ⁰ 123.55 ⁰ 1.5029 0.70 ⁰ 1.58 0.66 ⁰ 234.61 ⁰ 1.5368
360 ⁰ 1.3814 7.2619 687.0 1.58 317.09 ⁰ 124.24 ⁰ 1.5156 0.69 ⁰ 1.58 0.68 ⁰ 235.28 ⁰ 1.5243

incr.


1+ecosθ
𝑅(θ)²dθ

2
A

T
T-
Ti-1
0.9856°

day
Numerical
Methods
C1

1+eC1cosθ
θ-
θi-1
∆AC1∝ ∆t
∆tC1=∆tC2
∆t ∝∆AC2
θ-
θi-1
Numerical
Methods
C2

1+eC2cosθ