View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22565U 26041.92755235 +.00000000 +00000-0 -41577-4 0 00003
2 22565 70.7628 220.0457 0003125 102.4698 257.6771 14.12376199 01
| Epoch (UTC): | 10 February 2026 22:15:40 |
| Eccentricity: | 0.0003125 |
| inclination: | 70.7628° |
| perigee height: | 849 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 220.0457° |
| argument of perigee: | 102.4698° |
| revolutions per day: | 14.12376199 |
| mean anomaly at epoch: | 257.6771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|