View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62435U 26144.95444837 +.00000000 +00000-0 +99264-3 0 00007
2 62435 53.1603 341.1505 0001053 83.5967 276.5154 15.30206232 00
| Epoch (UTC): | 24 May 2026 22:54:24 |
| Eccentricity: | 0.0001053 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 341.1505° |
| argument of perigee: | 83.5967° |
| revolutions per day: | 15.30206232 |
| mean anomaly at epoch: | 276.5154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|