Initial orbit conditions of the remote sensing scenario
| Epoch: 2016.03.21 01:00:00.00 (GPS); Week Number: 865; GPS Seconds of Week: 90 000.0 | ||||
|---|---|---|---|---|
| Orbital Elements | Chief Spacecraft | Deputy Spacecraft | Relative State in Body Frame | |
| Semi-major axis a, m | 6 880 540 | 6 879 040 | Radial offset, m | -854.34 |
| Eccentricity e | 0.044 | 0.044 | In-track offset, m | -1.4978 × 104 |
| Inclination i, ° | 10 | 10 | Cross-track offset, m | 0.00 |
| Argument of perigee ω, ° | 180 | 180 | Radial relative velocity, m/s | -0.03 |
| Longitude of ascending node Ω, ° | 67.489 | 67.479 | In-track relative velocity, m/s | 1.76 |
| Mean anomaly M, ° | -90.000 | -90.125 | Cross-track relative velocity, m/s | 0.00 |