View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20793U 26088.23886633 +.00000000 +00000-0 +54778-3 0 00001
2 20793 98.7710 76.7780 0018346 204.6560 166.0486 14.20853530 07
| Epoch (UTC): | 29 March 2026 05:43:58 |
| Eccentricity: | 0.0018346 |
| inclination: | 98.7710° |
| perigee height: | 809 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 76.7780° |
| argument of perigee: | 204.6560° |
| revolutions per day: | 14.20853530 |
| mean anomaly at epoch: | 166.0486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|