View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41887U 26145.14689016 +.00000000 +00000-0 +31853-3 0 00007
2 41887 34.9410 54.2722 0008785 286.1793 73.7964 15.56158820 04
| Epoch (UTC): | 25 May 2026 03:31:31 |
| Eccentricity: | 0.0008785 |
| inclination: | 34.9410° |
| perigee height: | 393 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 54.2722° |
| argument of perigee: | 286.1793° |
| revolutions per day: | 15.56158820 |
| mean anomaly at epoch: | 73.7964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|