View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44793U 26144.45594983 +.00000000 +00000-0 +00000-0 0 00004
2 44793 53.9590 300.6620 0006957 49.8276 310.2109 1.86227016 09
| Epoch (UTC): | 24 May 2026 10:56:34 |
| Eccentricity: | 0.0006957 |
| inclination: | 53.9590° |
| perigee height: | 21509 km |
| apogee height: | 21548 km |
| right ascension of ascending node: | 300.6620° |
| argument of perigee: | 49.8276° |
| revolutions per day: | 1.86227016 |
| mean anomaly at epoch: | 310.2109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|