View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25544U 26158.90128686 +.00000000 +00000-0 +14961-3 0 00009
2 25544 51.6338 346.0598 0006926 145.2709 214.8733 15.49660544 06
| Epoch (UTC): | 07 June 2026 21:37:51 |
| Eccentricity: | 0.0006926 |
| inclination: | 51.6338° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 346.0598° |
| argument of perigee: | 145.2709° |
| revolutions per day: | 15.49660544 |
| mean anomaly at epoch: | 214.8733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|