View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53061U 26145.49256661 +.00000000 +00000-0 +24038-4 0 00006
2 53061 97.4476 325.4023 0001959 82.1060 278.0389 15.05651404 02
| Epoch (UTC): | 25 May 2026 11:49:17 |
| Eccentricity: | 0.0001959 |
| inclination: | 97.4476° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 325.4023° |
| argument of perigee: | 82.1060° |
| revolutions per day: | 15.05651404 |
| mean anomaly at epoch: | 278.0389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|