View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50827U 26145.39768522 +.00000000 +00000-0 -13265-5 0 00008
2 50827 53.2098 184.7666 0001403 82.9028 277.2123 15.08845524 02
| Epoch (UTC): | 25 May 2026 09:32:40 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.2098° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.7666° |
| argument of perigee: | 82.9028° |
| revolutions per day: | 15.08845524 |
| mean anomaly at epoch: | 277.2123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|