View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56129U 26145.00481534 +.00000000 +00000-0 +12184-3 0 00008
2 56129 43.0037 24.7717 0001465 260.0963 99.9724 15.27571960 05
| Epoch (UTC): | 25 May 2026 00:06:56 |
| Eccentricity: | 0.0001465 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 24.7717° |
| argument of perigee: | 260.0963° |
| revolutions per day: | 15.27571960 |
| mean anomaly at epoch: | 99.9724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|