View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57105U 26145.54204387 +.00000000 +00000-0 -29405-4 0 00007
2 57105 43.0031 207.7353 0000484 185.3637 174.7209 15.27581315 05
| Epoch (UTC): | 25 May 2026 13:00:32 |
| Eccentricity: | 0.0000484 |
| inclination: | 43.0031° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 207.7353° |
| argument of perigee: | 185.3637° |
| revolutions per day: | 15.27581315 |
| mean anomaly at epoch: | 174.7209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|