View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 50821U 26145.49703689 +.00000000 +00000-0 +44241-4 0 00002
2 50821 53.2144 184.2011 0001168 100.7229 259.3895 15.08833329 04
| Epoch (UTC): | 25 May 2026 11:55:43 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.2011° |
| argument of perigee: | 100.7229° |
| revolutions per day: | 15.08833329 |
| mean anomaly at epoch: | 259.3895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|