View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57531U 26145.43210091 +.00000000 +00000-0 -14196-3 0 00007
2 57531 43.0045 288.5861 0001388 275.7560 84.3133 15.27599940 02
| Epoch (UTC): | 25 May 2026 10:22:13 |
| Eccentricity: | 0.0001388 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 288.5861° |
| argument of perigee: | 275.7560° |
| revolutions per day: | 15.27599940 |
| mean anomaly at epoch: | 84.3133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|