View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57458U 26145.35648601 +.00000000 +00000-0 +16043-4 0 00001
2 57458 43.0016 266.4271 0001234 279.1378 80.9334 15.27577699 05
| Epoch (UTC): | 25 May 2026 08:33:20 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.4271° |
| argument of perigee: | 279.1378° |
| revolutions per day: | 15.27577699 |
| mean anomaly at epoch: | 80.9334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|