View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54864U 26145.43125897 +.00000000 +00000-0 -11315-3 0 00002
2 54864 43.0039 48.4830 0001257 241.8386 118.2339 15.27551414 04
| Epoch (UTC): | 25 May 2026 10:21:00 |
| Eccentricity: | 0.0001257 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.4830° |
| argument of perigee: | 241.8386° |
| revolutions per day: | 15.27551414 |
| mean anomaly at epoch: | 118.2339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|