View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56010U 26145.28758646 +.00000000 +00000-0 +15523-4 0 00009
2 56010 43.0052 347.0547 0001660 272.0558 88.0103 15.27577006 00
| Epoch (UTC): | 25 May 2026 06:54:07 |
| Eccentricity: | 0.0001660 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 347.0547° |
| argument of perigee: | 272.0558° |
| revolutions per day: | 15.27577006 |
| mean anomaly at epoch: | 88.0103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|