View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57108U 26145.46123885 +.00000000 +00000-0 -50796-5 0 00002
2 57108 43.0025 207.9829 0001211 270.7009 89.3704 15.27574314 04
| Epoch (UTC): | 25 May 2026 11:04:11 |
| Eccentricity: | 0.0001211 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.9829° |
| argument of perigee: | 270.7009° |
| revolutions per day: | 15.27574314 |
| mean anomaly at epoch: | 89.3704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|