View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16882U 26100.05405373 +.00000000 +00000-0 +48188-4 0 00007
2 16882 82.5168 97.1837 0017726 225.0041 195.5434 14.85673218 05
| Epoch (UTC): | 10 April 2026 01:17:50 |
| Eccentricity: | 0.0017726 |
| inclination: | 82.5168° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 97.1837° |
| argument of perigee: | 225.0041° |
| revolutions per day: | 14.85673218 |
| mean anomaly at epoch: | 195.5434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|