View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24920U 26145.46884564 +.00000000 +00000-0 +82091-4 0 00007
2 24920 69.9540 65.3350 0024173 305.0344 54.8509 14.27934587 01
| Epoch (UTC): | 25 May 2026 11:15:08 |
| Eccentricity: | 0.0024173 |
| inclination: | 69.9540° |
| perigee height: | 781 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 65.3350° |
| argument of perigee: | 305.0344° |
| revolutions per day: | 14.27934587 |
| mean anomaly at epoch: | 54.8509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|