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