View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61626U 26145.51515466 +.00000000 +00000-0 -16158-5 0 00002
2 61626 43.0003 84.2905 0000812 257.5856 102.4905 15.27575851 07
| Epoch (UTC): | 25 May 2026 12:21:49 |
| Eccentricity: | 0.0000812 |
| inclination: | 43.0003° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.2905° |
| argument of perigee: | 257.5856° |
| revolutions per day: | 15.27575851 |
| mean anomaly at epoch: | 102.4905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|