View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58540U 26145.50816515 +.00000000 +00000-0 -93528-4 0 00006
2 58540 53.1628 65.4289 0001244 82.2629 277.8515 15.34408268 09
| Epoch (UTC): | 25 May 2026 12:11:45 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.1628° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 65.4289° |
| argument of perigee: | 82.2629° |
| revolutions per day: | 15.34408268 |
| mean anomaly at epoch: | 277.8515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|