View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62450U 26145.25886150 +.00000000 +00000-0 +58926-3 0 00006
2 62450 53.1602 339.4919 0001233 87.8680 272.2462 15.30202363 00
| Epoch (UTC): | 25 May 2026 06:12:45 |
| Eccentricity: | 0.0001233 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 339.4919° |
| argument of perigee: | 87.8680° |
| revolutions per day: | 15.30202363 |
| mean anomaly at epoch: | 272.2462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|