View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64006U 26145.41576902 +.00000000 +00000-0 +11225-2 0 00004
2 64006 42.9992 284.2943 0002063 286.3137 73.7487 15.27589810 08
| Epoch (UTC): | 25 May 2026 09:58:42 |
| Eccentricity: | 0.0002063 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 284.2943° |
| argument of perigee: | 286.3137° |
| revolutions per day: | 15.27589810 |
| mean anomaly at epoch: | 73.7487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|