View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24285U 26161.41422872 +.00000000 +00000-0 +46415-3 0 00003
2 24285 82.9506 46.1147 1735960 122.7905 255.2481 11.82999359 06
| Epoch (UTC): | 10 June 2026 09:56:29 |
| Eccentricity: | 0.1735960 |
| inclination: | 82.9506° |
| perigee height: | 346 km |
| apogee height: | 3170 km |
| right ascension of ascending node: | 46.1147° |
| argument of perigee: | 122.7905° |
| revolutions per day: | 11.82999359 |
| mean anomaly at epoch: | 255.2481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|