View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54865U 26145.01322036 +.00000000 +00000-0 +12110-4 0 00005
2 54865 43.0046 50.5149 0001341 260.6039 99.4661 15.27577125 03
| Epoch (UTC): | 25 May 2026 00:19:02 |
| Eccentricity: | 0.0001341 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 50.5149° |
| argument of perigee: | 260.6039° |
| revolutions per day: | 15.27577125 |
| mean anomaly at epoch: | 99.4661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|