View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59284U 26145.59274872 +.00000000 +00000-0 +79721-4 0 00003
2 59284 50.0114 58.5314 0012044 339.4741 20.5689 14.27955195 07
| Epoch (UTC): | 25 May 2026 14:13:33 |
| Eccentricity: | 0.0012044 |
| inclination: | 50.0114° |
| perigee height: | 790 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 58.5314° |
| argument of perigee: | 339.4741° |
| revolutions per day: | 14.27955195 |
| mean anomaly at epoch: | 20.5689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|