View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58035U 26145.52571031 +.00000000 +00000-0 -47502-4 0 00009
2 58035 53.1609 81.2112 0001392 91.7717 268.3443 15.30182671 03
| Epoch (UTC): | 25 May 2026 12:37:01 |
| Eccentricity: | 0.0001392 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.2112° |
| argument of perigee: | 91.7717° |
| revolutions per day: | 15.30182671 |
| mean anomaly at epoch: | 268.3443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|