View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65477U 26145.33335647 +.00000000 +00000-0 +88278-3 0 00000
2 65477 53.1597 262.2084 0001020 95.9003 50.6575 15.34376450 00
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001020 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 262.2084° |
| argument of perigee: | 95.9003° |
| revolutions per day: | 15.34376450 |
| mean anomaly at epoch: | 50.6575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|