View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57136U 26145.56859370 +.00000000 +00000-0 -30697-5 0 00007
2 57136 43.0026 188.9510 0001337 289.0158 71.0549 15.27575210 09
| Epoch (UTC): | 25 May 2026 13:38:46 |
| Eccentricity: | 0.0001337 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 188.9510° |
| argument of perigee: | 289.0158° |
| revolutions per day: | 15.27575210 |
| mean anomaly at epoch: | 71.0549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|