View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58839U 26145.56058301 +.00000000 +00000-0 +17191-4 0 00005
2 58839 53.1606 196.7411 0001117 77.2730 282.8397 15.34388979 07
| Epoch (UTC): | 25 May 2026 13:27:14 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 196.7411° |
| argument of perigee: | 77.2730° |
| revolutions per day: | 15.34388979 |
| mean anomaly at epoch: | 282.8397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|