View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58112U 26145.45743683 +.00000000 +00000-0 +13114-4 0 00002
2 58112 53.1596 169.0530 0001124 82.2321 277.8808 15.30190653 01
| Epoch (UTC): | 25 May 2026 10:58:42 |
| Eccentricity: | 0.0001124 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.0530° |
| argument of perigee: | 82.2321° |
| revolutions per day: | 15.30190653 |
| mean anomaly at epoch: | 277.8808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|