View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65691U 26145.53067583 +.00000000 +00000-0 +68791-3 0 00009
2 65691 53.1612 338.3785 0001314 98.3367 261.7783 15.30216341 09
| Epoch (UTC): | 25 May 2026 12:44:10 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.3785° |
| argument of perigee: | 98.3367° |
| revolutions per day: | 15.30216341 |
| mean anomaly at epoch: | 261.7783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|