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What orbits around Earth has the least and most sun light exposure?

I wondered: When taking pictures either of Earth or otherwise with various telescopes in orbit, does it help to be in Earth's shadow?

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As @OrganicMarble suggests a nice Sun-synchronous orbit is probably the answer to both "least" and "most".

Sun-synchronous orbits around the Earth are often used to keep satellites over areas of the Earth that happen to be in constant sunlight for photographic reasons, and a side benefit can be that there is constant sunlight available for the satellite's solar panels.

So I've just asked "Satellites that take advantage of, or require constant availability of sunlight on the spacecraft itself, available in Sun-synchronous orbits?

note 1: Halo orbits around the Sun-Earth Lagrange points are really heliocentric orbits in 1:1 resonance with Earth, but I'm counting them for educational purposes. You may discount them to taste.

note 2: Halo orbits around the Earth-Moon Lagrange points are really geocentric Earth orbits in 1:1 resonance with the Moon, so they really do count!


As for least Sun, I can think of several options:

  1. Elliptical Sun-synchronous orbit with apogee in the Earth's shadow. The more eccentric, the more susceptible to long term perturbations from the Sun and Moon that would eventually require station-keeping.
  2. Nothing like a Sun-synchronous orbit is available around the Moon. Any lunar orbit at all is tricky due to lumpy gravity (mascons) but since the Moon is quite spherical compared to the oblate Earth, there's no J2 with which to precess the nodes.
  3. Tiny halo orbit associated with Sun-Earth L2 (behind the Earth), although a) it's unstable and would require a lot of station-keeping and b) it would only offer partial relief from Sunlight (partial eclipse in the Earth's ant-umbra) most of the time.

  4. update: Wrong! See @Lex's comment, good catch Lex! Tiny halo orbit associated with Earth-Moon L2 (behind the Moon), although a) it's unstable and would require a lot of station-keeping and b) it would offer complete relief from Sunlight (partial eclipse in the Moon's ant-umbra)

enter image description here

Some approximate numbers:

a_Earth:           149598023  km
Sun-Earth L1:      1491598  km
Sun-Earth L2:      1501579  km
Earth r_Hill:      1496606  km
d_antumbra_Earth:  1382778  km

a_Moon:           384400  km
Earth-Moon L1:    58023  km
Earth-Moon L2:    64520  km
Moon r_Hill:      61529  km
d_antumbra_Moon:  374073  km

A Python script for the numbers and plot:

def solve_L1 (r, R, M1, M2):
    return M2/r**2 + M1/R**2 - r*(M1 + M2)/R**3 - M1/(R-r)**2

def solve_L2 (r, R, M1, M2):
    return M1/R**2 + r*(M1 + M2)/R**3 - M1/(R+r)**2 - M2/r**2

def r_Hill(R, M1, M2):
    return R * (M2 / (3.*M1))**(1./3.)

import numpy as np
import matplotlib.pyplot as plt
from scipy.optimize import brentq

a_Earth  = 149598023.   # Earth's semi-major axis (km)
a_Moon   = 384400.      # Moon's   semi-major axis (km)

r_Sun   =        696392.  # Earth's radius (km)
r_Earth =          6378.  # Earth's radius (km)
r_Moon  =          1737.  # Moon's radius (km)

r_low_Earth    =   1480000.   #  (lower guess, km)
r_high_Earth   =   1510000.   #  (upper guess, km)

r_low_Moon    =   55000.   #  (lower guess, km)
r_high_Moon   =   70000.   #  (upper guess, km)

GM_Sun    = 1.327E+20  # approximate  (m^3/s^2)
GM_Earth  = 3.986E+14  # approximate  (m^3/s^2)
GM_Moon   = 4.904E+12  # approximate  (m^3/s^2)

r_Hill_Earth = r_Hill(a_Earth, GM_Sun, GM_Earth)

r_Hill_Moon  = r_Hill(a_Moon, GM_Earth, GM_Moon)

d_antumbra_Earth = a_Earth * ((r_Sun / (r_Sun - r_Earth)) - 1.)
d_antumbra_Moon  = a_Earth * ((r_Sun / (r_Sun - r_Moon )) - 1.)

r_L1_Earth = brentq(solve_L1, r_low_Earth, r_high_Earth,
                    args=(a_Earth, GM_Sun, GM_Earth))

r_L2_Earth = brentq(solve_L2, r_low_Earth, r_high_Earth,
                    args=(a_Earth, GM_Sun, GM_Earth))

r_L1_Moon = brentq(solve_L1, r_low_Moon, r_high_Moon,
                    args=(a_Moon, GM_Earth, GM_Moon))

r_L2_Moon = brentq(solve_L2, r_low_Moon, r_high_Moon,
                    args=(a_Moon, GM_Earth, GM_Moon))

if True:
    plt.figure()

    plt.subplot(2, 1, 1)

    r = np.linspace(r_low_Earth, r_high_Earth)
    plt.plot(r, solve_L1(r, a_Earth, GM_Sun, GM_Earth),  '-g')
    plt.plot(r, solve_L2(r, a_Earth, GM_Sun, GM_Earth), '--g')
    plt.plot([r_Hill_Earth], [0], 'ok')
    plt.plot([r_L1_Earth], [0], 'ok')
    plt.plot([r_L2_Earth], [0], 'ok')
    plt.plot(r, np.zeros_like(r), '-k')

    plt.text(1491000,  +3, 'L1',          fontsize=14)
    plt.text(1496000,  +3, 'Hill',          fontsize=14)
    plt.text(1501000,  +3, 'L2',          fontsize=14)

    plt.subplot(2, 1, 2)

    r = np.linspace(r_low_Moon, r_high_Moon)
    plt.plot(r, solve_L1(r, a_Moon, GM_Earth, GM_Moon),  '-g')
    plt.plot(r, solve_L2(r, a_Moon, GM_Earth, GM_Moon), '--g')
    plt.plot([r_Hill_Moon], [0], 'ok')
    plt.plot([r_L1_Moon], [0], 'ok')
    plt.plot([r_L2_Moon], [0], 'ok')
    plt.plot(r, np.zeros_like(r), '-k')

    plt.text(58000,  +100, 'L1', fontsize=14)
    plt.text(61000,  +100, 'Hill', fontsize=14)
    plt.text(64000,  +100, 'L2', fontsize=14)

    plt.ylim(-300, 300)

    plt.show()
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  • $\begingroup$ As for "tiny halo orbits", see the many answers to Are large halo orbits around L₁'s and L₂'s preferred over small orbits for reasons other than geometry? thought I think there's a station-keeping expense answer that hasn't been written yet. $\endgroup$ – uhoh Nov 21 '18 at 23:57
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    $\begingroup$ I am pretty sure that 4 is wrong. Earth-Moon L2 is behind the moon with respect to Earth, but not the sun. This would be shadowed from Earth radio waves all the time, but only shadowed from the sun during a full moon. $\endgroup$ – Lex Nov 22 '18 at 1:19
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    $\begingroup$ @Lex Ha! you are absolutely right. I hadn't had my morning coffee yet. How does that look? $\endgroup$ – uhoh Nov 22 '18 at 1:23

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