View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68088U 26145.37876605 +.00000000 +00000-0 +65980-3 0 00004
2 68088 53.1587 182.0198 0001086 74.6804 285.4319 15.34410704 05
| Epoch (UTC): | 25 May 2026 09:05:25 |
| Eccentricity: | 0.0001086 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 182.0198° |
| argument of perigee: | 74.6804° |
| revolutions per day: | 15.34410704 |
| mean anomaly at epoch: | 285.4319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|