View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62048U 26145.59944404 +.00000000 +00000-0 +48389-3 0 00005
2 62048 42.9996 189.2700 0001654 275.9196 84.1467 15.27591482 07
| Epoch (UTC): | 25 May 2026 14:23:11 |
| Eccentricity: | 0.0001654 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.2700° |
| argument of perigee: | 275.9196° |
| revolutions per day: | 15.27591482 |
| mean anomaly at epoch: | 84.1467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|