Options for Staging Orbits in Cis-Lunar Space 20150019648

20150019648 Johnson Space Center STI

Near-rectilinear halo orbit

PE 3,000 AP 7,000

Prograde Circular Orbit

PE 3,000 AP 7,000

Orbit Period 11 hrs
Lunar (or L-point) Amplitude Range
3,000 to 5,000 km
E-M Orientation
∼ 75 ◦ inclination

Prograde Circular Orbits (PCOs) are defined in this paper as circular orbits of various sizes that rotate in the prograde

direction and are highly stable, requiring few to 0 corrections to be maintained. Frozen orbits are similar but need not be circular and have orbital parameters that oscillate around fixed values. Highly stable and/or frozen orbits have been discovered for both the Earth [13] [14] and Moon [15] [16]. Frozen orbits are generally discovered by analyzing unique aspects of the gravitational potential and finding regions of behavior that lend themselves to canceling the effects of shape irregularities.

Data Update

Emergency Update

Must follow the procedure immediately. Prepare to make an emergency evacuation from the Lunar Gateway.

Data From NASA Goddard Space Flight Center