View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65810U 26040.51902436 +.00000000 +00000-0 +50829-3 0 00002
2 65810 97.6013 265.2329 0002266 86.3997 273.7489 15.05670851 03
| Epoch (UTC): | 09 February 2026 12:27:23 |
| Eccentricity: | 0.0002266 |
| inclination: | 97.6013° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 265.2329° |
| argument of perigee: | 86.3997° |
| revolutions per day: | 15.05670851 |
| mean anomaly at epoch: | 273.7489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|