View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20625U 90046B 25189.17031384 -.00000107 00000-0 -30365-4 0 9997
2 20625 71.0002 91.4286 0016009 310.4113 49.5612 14.14971787814050
| Epoch (UTC): | 08 July 2025 04:05:15 |
| Eccentricity: | 0.0016009 |
| inclination: | 71.0002° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 91.4286° |
| argument of perigee: | 310.4113° |
| revolutions per day: | 14.14971787 |
| mean anomaly at epoch: | 49.5612° |
| orbit number at epoch: | 81405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|