View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55452U 26145.36822485 +.00000000 +00000-0 -22801-5 0 00009
2 55452 43.0022 256.1396 0001938 282.9872 77.0763 15.27573247 08
| Epoch (UTC): | 25 May 2026 08:50:14 |
| Eccentricity: | 0.0001938 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 256.1396° |
| argument of perigee: | 282.9872° |
| revolutions per day: | 15.27573247 |
| mean anomaly at epoch: | 77.0763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|