View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48958U 26145.47633433 +.00000000 +00000-0 +28992-3 0 00001
2 48958 97.6877 337.7742 0007568 67.3124 292.8929 15.55210457 08
| Epoch (UTC): | 25 May 2026 11:25:55 |
| Eccentricity: | 0.0007568 |
| inclination: | 97.6877° |
| perigee height: | 396 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 337.7742° |
| argument of perigee: | 67.3124° |
| revolutions per day: | 15.55210457 |
| mean anomaly at epoch: | 292.8929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|