Table 4
Achievable orbital shape after recovery with respect to different periapsis altitudes when the overall RM magnitude is limited to 0.863 km/s
| Periapsis altitudes |
| 30 | 50 | 100 | 200 | 300 | 500 | 1,000 |
| TOF Leg 1 (hour) | 5.00 | 5.00 | 5.00 | 5.00 | 5.00 | 5.00 | 4.91 |
| TOF Leg 2 (days) | 5.25 | 5.25 | 5.25 | 5.25 | 5.25 | 5.25 | 5.32 |
| RM #1 Mag. (km/s) | 0.654 | 0.654 | 0.655 | 0.657 | 0.658 | 0.662 | 0.667 |
| RM #2 Mag. (km/s) | 0.209 | 0.209 | 0.208 | 0.206 | 0.205 | 0.201 | 0.196 |
| Semi major axis (km) | 4,574.738 | 4,603.837 | 4,676.338 | 4,820.391 | 4,963.383 | 5,247.026 | 5,867.997 |
| Eccentricity | 0.60938 | 0.60747 | 0.60278 | 0.59376 | 0.58517 | 0.56924 | 0.52857 |
| Period (hour) | 7.743 | 7.817 | 8.002 | 8.374 | 8.749 | 9.508 | 11.248 |
| Apoapsis altitude (km) | 5,643.477 | 5,681.675 | 5,776.676 | 5,964.782 | 6,150.766 | 6,518.052 | 7,259.995 |