View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24827U 26071.93685845 +.00000000 +00000-0 +41971-3 0 00005
2 24827 63.3113 7.3243 1089605 68.4992 11.4366 11.07980118 05
| Epoch (UTC): | 12 March 2026 22:29:04 |
| Eccentricity: | 0.1089605 |
| inclination: | 63.3113° |
| perigee height: | 1195 km |
| apogee height: | 3047 km |
| right ascension of ascending node: | 7.3243° |
| argument of perigee: | 68.4992° |
| revolutions per day: | 11.07980118 |
| mean anomaly at epoch: | 11.4366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|