View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58795U 26145.55392753 +.00000000 +00000-0 +15557-5 0 00002
2 58795 43.0021 90.9663 0000731 275.6712 84.4056 15.27574316 08
| Epoch (UTC): | 25 May 2026 13:17:39 |
| Eccentricity: | 0.0000731 |
| inclination: | 43.0021° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 90.9663° |
| argument of perigee: | 275.6712° |
| revolutions per day: | 15.27574316 |
| mean anomaly at epoch: | 84.4056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|