View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62962U 26145.50820442 +.00000000 +00000-0 +56819-3 0 00003
2 62962 53.1598 235.3025 0001707 95.2695 264.8500 15.30208911 04
| Epoch (UTC): | 25 May 2026 12:11:48 |
| Eccentricity: | 0.0001707 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.3025° |
| argument of perigee: | 95.2695° |
| revolutions per day: | 15.30208911 |
| mean anomaly at epoch: | 264.8500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|