View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65584U 26145.38471685 +.00000000 +00000-0 +78343-4 0 00000
2 65584 81.3038 31.8304 0006419 246.6839 113.3642 13.83797772 04
| Epoch (UTC): | 25 May 2026 09:13:59 |
| Eccentricity: | 0.0006419 |
| inclination: | 81.3038° |
| perigee height: | 946 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 31.8304° |
| argument of perigee: | 246.6839° |
| revolutions per day: | 13.83797772 |
| mean anomaly at epoch: | 113.3642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|