View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22825U 93061C 23338.82289683 .00000222 00000-0 10316-3 0 9993
2 22825 98.8193 24.2785 0007399 292.5675 67.4724 14.30391091574682
| Epoch (UTC): | 04 December 2023 19:44:58 |
| Eccentricity: | 0.0007399 |
| inclination: | 98.8193° |
| perigee height: | 785 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 24.2785° |
| argument of perigee: | 292.5675° |
| revolutions per day: | 14.30391091 |
| mean anomaly at epoch: | 67.4724° |
| orbit number at epoch: | 57468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|