View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00117U 26088.01610263 +.00000000 +00000-0 +29330-4 0 00006
2 00117 66.8127 200.5950 0078837 349.0487 10.8871 13.90181578 08
| Epoch (UTC): | 29 March 2026 00:23:11 |
| Eccentricity: | 0.0078837 |
| inclination: | 66.8127° |
| perigee height: | 870 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 200.5950° |
| argument of perigee: | 349.0487° |
| revolutions per day: | 13.90181578 |
| mean anomaly at epoch: | 10.8871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|