View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52682U 26145.46070505 +.00000000 +00000-0 -35400-6 0 00000
2 52682 53.2138 159.4813 0001266 75.7627 284.3505 15.08836721 05
| Epoch (UTC): | 25 May 2026 11:03:24 |
| Eccentricity: | 0.0001266 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 159.4813° |
| argument of perigee: | 75.7627° |
| revolutions per day: | 15.08836721 |
| mean anomaly at epoch: | 284.3505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|