View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65496U 26145.33719124 +.00000000 +00000-0 +52704-3 0 00002
2 65496 53.1596 275.0839 0001213 86.8149 273.2991 15.30211894 05
| Epoch (UTC): | 25 May 2026 08:05:33 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 275.0839° |
| argument of perigee: | 86.8149° |
| revolutions per day: | 15.30211894 |
| mean anomaly at epoch: | 273.2991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|