View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57256U 26145.47852639 +.00000000 +00000-0 +63793-4 0 00002
2 57256 43.0033 306.2508 0001315 275.6021 84.4680 15.27584372 01
| Epoch (UTC): | 25 May 2026 11:29:04 |
| Eccentricity: | 0.0001315 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.2508° |
| argument of perigee: | 275.6021° |
| revolutions per day: | 15.27584372 |
| mean anomaly at epoch: | 84.4680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|