View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57896U 26145.56483231 +.00000000 +00000-0 +79979-4 0 00003
2 57896 42.9988 240.0242 0001244 263.0916 96.9794 15.27578492 03
| Epoch (UTC): | 25 May 2026 13:33:21 |
| Eccentricity: | 0.0001244 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.0242° |
| argument of perigee: | 263.0916° |
| revolutions per day: | 15.27578492 |
| mean anomaly at epoch: | 96.9794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|