View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56876U 26145.03317657 +.00000000 +00000-0 +21125-4 0 00000
2 56876 43.0072 14.2670 0001544 267.1641 92.9034 15.27579118 04
| Epoch (UTC): | 25 May 2026 00:47:46 |
| Eccentricity: | 0.0001544 |
| inclination: | 43.0072° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 14.2670° |
| argument of perigee: | 267.1641° |
| revolutions per day: | 15.27579118 |
| mean anomaly at epoch: | 92.9034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|