View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53807U 26038.82241911 +.00000000 +00000-0 +19458-3 0 00003
2 53807 53.2287 280.5995 0007989 127.5086 232.6646 15.36705062 06
| Epoch (UTC): | 07 February 2026 19:44:17 |
| Eccentricity: | 0.0007989 |
| inclination: | 53.2287° |
| perigee height: | 450 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 280.5995° |
| argument of perigee: | 127.5086° |
| revolutions per day: | 15.36705062 |
| mean anomaly at epoch: | 232.6646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|