View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22803U 26041.44425696 +.00000000 +00000-0 +40157-4 0 00002
2 22803 70.9891 68.5836 0019493 254.0311 105.8666 14.17228082 06
| Epoch (UTC): | 10 February 2026 10:39:43 |
| Eccentricity: | 0.0019493 |
| inclination: | 70.9891° |
| perigee height: | 821 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 68.5836° |
| argument of perigee: | 254.0311° |
| revolutions per day: | 14.17228082 |
| mean anomaly at epoch: | 105.8666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|