View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68863U 26145.58335647 +.00000000 +00000-0 +74255-3 0 00009
2 68863 97.2851 160.3092 0000765 105.9160 187.9701 15.49166325 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000765 |
| inclination: | 97.2851° |
| perigee height: | 419 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.3092° |
| argument of perigee: | 105.9160° |
| revolutions per day: | 15.49166325 |
| mean anomaly at epoch: | 187.9701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|