View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65896U 26145.34214927 +.00000000 +00000-0 +38373-3 0 00004
2 65896 53.1596 15.0509 0001579 73.5833 286.5342 15.31714800 06
| Epoch (UTC): | 25 May 2026 08:12:41 |
| Eccentricity: | 0.0001579 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 15.0509° |
| argument of perigee: | 73.5833° |
| revolutions per day: | 15.31714800 |
| mean anomaly at epoch: | 286.5342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|