View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 06660U 26088.22033654 +.00000000 +00000-0 +28635-5 0 00009
2 06660 81.2299 140.3946 0047965 78.5688 282.0863 14.06269655 04
| Epoch (UTC): | 29 March 2026 05:17:17 |
| Eccentricity: | 0.0047965 |
| inclination: | 81.2299° |
| perigee height: | 837 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 140.3946° |
| argument of perigee: | 78.5688° |
| revolutions per day: | 14.06269655 |
| mean anomaly at epoch: | 282.0863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|