View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55501U 26144.75276404 +.00000000 +00000-0 +11838-3 0 00005
2 55501 43.0034 270.5312 0001545 263.1289 96.9387 15.27573038 01
| Epoch (UTC): | 24 May 2026 18:03:58 |
| Eccentricity: | 0.0001545 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.5312° |
| argument of perigee: | 263.1289° |
| revolutions per day: | 15.27573038 |
| mean anomaly at epoch: | 96.9387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|