View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56922U 26145.31450289 +.00000000 +00000-0 +52849-5 0 00000
2 56922 43.0039 358.2220 0001782 277.1134 82.9515 15.27575463 05
| Epoch (UTC): | 25 May 2026 07:32:53 |
| Eccentricity: | 0.0001782 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 358.2220° |
| argument of perigee: | 277.1134° |
| revolutions per day: | 15.27575463 |
| mean anomaly at epoch: | 82.9515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|