View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54760U 26145.17920662 +.00000000 +00000-0 -75167-4 0 00007
2 54760 53.2144 60.9325 0001823 91.6071 268.5130 15.08848739 04
| Epoch (UTC): | 25 May 2026 04:18:03 |
| Eccentricity: | 0.0001823 |
| inclination: | 53.2144° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 60.9325° |
| argument of perigee: | 91.6071° |
| revolutions per day: | 15.08848739 |
| mean anomaly at epoch: | 268.5130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|