View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49282U 26145.37536652 +.00000000 +00000-0 -21261-3 0 00009
2 49282 87.8944 294.2536 0001756 89.5941 270.5390 13.14502079 01
| Epoch (UTC): | 25 May 2026 09:00:31 |
| Eccentricity: | 0.0001756 |
| inclination: | 87.8944° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2536° |
| argument of perigee: | 89.5941° |
| revolutions per day: | 13.14502079 |
| mean anomaly at epoch: | 270.5390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|