View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62021U 26145.45596447 +.00000000 +00000-0 +34924-3 0 00001
2 62021 53.1587 171.8662 0001111 85.5904 274.5224 15.30203190 08
| Epoch (UTC): | 25 May 2026 10:56:35 |
| Eccentricity: | 0.0001111 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.8662° |
| argument of perigee: | 85.5904° |
| revolutions per day: | 15.30203190 |
| mean anomaly at epoch: | 274.5224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|