View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57785U 26145.36957227 +.00000000 +00000-0 +54472-4 0 00000
2 57785 43.0036 121.3724 0001322 279.0356 81.0346 15.27578219 09
| Epoch (UTC): | 25 May 2026 08:52:11 |
| Eccentricity: | 0.0001322 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.3724° |
| argument of perigee: | 279.0356° |
| revolutions per day: | 15.27578219 |
| mean anomaly at epoch: | 81.0346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|