View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56551U 26145.46854777 +.00000000 +00000-0 +13993-4 0 00000
2 56551 43.0039 150.0434 0001377 290.1471 69.9233 15.27577677 08
| Epoch (UTC): | 25 May 2026 11:14:42 |
| Eccentricity: | 0.0001377 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.0434° |
| argument of perigee: | 290.1471° |
| revolutions per day: | 15.27577677 |
| mean anomaly at epoch: | 69.9233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|