View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50819U 26145.40872675 +.00000000 +00000-0 -18986-3 0 00009
2 50819 53.2098 184.7163 0000980 95.6829 264.4275 15.08851806 00
| Epoch (UTC): | 25 May 2026 09:48:33 |
| Eccentricity: | 0.0000980 |
| inclination: | 53.2098° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 184.7163° |
| argument of perigee: | 95.6829° |
| revolutions per day: | 15.08851806 |
| mean anomaly at epoch: | 264.4275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|