View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68935U 26145.49689487 +.00000000 +00000-0 +39971-3 0 00009
2 68935 51.8769 177.6719 0019945 74.9482 285.3707 15.30644496 03
| Epoch (UTC): | 25 May 2026 11:55:31 |
| Eccentricity: | 0.0019945 |
| inclination: | 51.8769° |
| perigee height: | 460 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 177.6719° |
| argument of perigee: | 74.9482° |
| revolutions per day: | 15.30644496 |
| mean anomaly at epoch: | 285.3707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|