View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24971U 26150.42628311 +.00000000 +00000-0 +53237-4 0 00001
2 24971 98.8423 144.3926 0050952 280.5781 78.9666 14.35507344 08
| Epoch (UTC): | 30 May 2026 10:13:50 |
| Eccentricity: | 0.0050952 |
| inclination: | 98.8423° |
| perigee height: | 737 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 144.3926° |
| argument of perigee: | 280.5781° |
| revolutions per day: | 14.35507344 |
| mean anomaly at epoch: | 78.9666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|