View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54862U 26145.07732950 +.00000000 +00000-0 -34557-4 0 00008
2 54862 43.0065 50.1560 0001442 252.3574 107.7121 15.27572242 07
| Epoch (UTC): | 25 May 2026 01:51:21 |
| Eccentricity: | 0.0001442 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 50.1560° |
| argument of perigee: | 252.3574° |
| revolutions per day: | 15.27572242 |
| mean anomaly at epoch: | 107.7121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|