View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31793U 26064.75543352 +.00000000 +00000-0 -24594-4 0 00007
2 31793 70.9757 180.6541 0002372 277.2484 192.7201 14.14833448 05
| Epoch (UTC): | 05 March 2026 18:07:49 |
| Eccentricity: | 0.0002372 |
| inclination: | 70.9757° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 180.6541° |
| argument of perigee: | 277.2484° |
| revolutions per day: | 14.14833448 |
| mean anomaly at epoch: | 192.7201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|