View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62835U 26145.55427628 +.00000000 +00000-0 +12717-2 0 00004
2 62835 43.0019 203.1967 0005388 246.7510 113.2791 15.70881920 05
| Epoch (UTC): | 25 May 2026 13:18:09 |
| Eccentricity: | 0.0005388 |
| inclination: | 43.0019° |
| perigee height: | 353 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 203.1967° |
| argument of perigee: | 246.7510° |
| revolutions per day: | 15.70881920 |
| mean anomaly at epoch: | 113.2791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|