View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57810U 26145.48119694 +.00000000 +00000-0 +49530-3 0 00008
2 57810 43.0030 160.4166 0001526 265.6863 94.3815 15.27596884 02
| Epoch (UTC): | 25 May 2026 11:32:55 |
| Eccentricity: | 0.0001526 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.4166° |
| argument of perigee: | 265.6863° |
| revolutions per day: | 15.27596884 |
| mean anomaly at epoch: | 94.3815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|