View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65517U 26145.55482280 +.00000000 +00000-0 +55463-3 0 00005
2 65517 53.1599 272.8858 0000816 42.3331 317.7734 15.34392287 05
| Epoch (UTC): | 25 May 2026 13:18:56 |
| Eccentricity: | 0.0000816 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 272.8858° |
| argument of perigee: | 42.3331° |
| revolutions per day: | 15.34392287 |
| mean anomaly at epoch: | 317.7734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|