View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62752U 26145.52461705 +.00000000 +00000-0 +58746-3 0 00006
2 62752 43.0017 80.8671 0001133 259.0221 101.0503 15.27603920 03
| Epoch (UTC): | 25 May 2026 12:35:26 |
| Eccentricity: | 0.0001133 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.8671° |
| argument of perigee: | 259.0221° |
| revolutions per day: | 15.27603920 |
| mean anomaly at epoch: | 101.0503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|