View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00117U 26047.15242709 +.00000000 +00000-0 +79696-4 0 00002
2 00117 66.8130 300.2175 0075438 17.7910 342.5783 13.90176255 06
| Epoch (UTC): | 16 February 2026 03:39:29 |
| Eccentricity: | 0.0075438 |
| inclination: | 66.8130° |
| perigee height: | 873 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 300.2175° |
| argument of perigee: | 17.7910° |
| revolutions per day: | 13.90176255 |
| mean anomaly at epoch: | 342.5783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|