View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51871U 26145.38665046 +.00000000 +00000-0 +16006-3 0 00007
2 51871 53.2138 24.8160 0001377 84.2922 275.8228 15.08833827 01
| Epoch (UTC): | 25 May 2026 09:16:46 |
| Eccentricity: | 0.0001377 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 24.8160° |
| argument of perigee: | 84.2922° |
| revolutions per day: | 15.08833827 |
| mean anomaly at epoch: | 275.8228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|