View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65357U 26145.58335647 +.00000000 +00000-0 +10883-2 0 00000
2 65357 53.1572 171.0767 0001209 79.9645 47.6312 15.30182997 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001209 |
| inclination: | 53.1572° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.0767° |
| argument of perigee: | 79.9645° |
| revolutions per day: | 15.30182997 |
| mean anomaly at epoch: | 47.6312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|