View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66800U 26145.39230373 +.00000000 +00000-0 +88624-3 0 00002
2 66800 43.0040 40.8545 0001843 280.6460 79.4185 15.27625847 02
| Epoch (UTC): | 25 May 2026 09:24:55 |
| Eccentricity: | 0.0001843 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.8545° |
| argument of perigee: | 280.6460° |
| revolutions per day: | 15.27625847 |
| mean anomaly at epoch: | 79.4185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|