View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11416U 26070.99125869 +.00000000 +00000-0 +12862-3 0 00002
2 11416 98.5747 101.1308 0009858 180.0463 180.0724 14.35435372 00
| Epoch (UTC): | 11 March 2026 23:47:24 |
| Eccentricity: | 0.0009858 |
| inclination: | 98.5747° |
| perigee height: | 767 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 101.1308° |
| argument of perigee: | 180.0463° |
| revolutions per day: | 14.35435372 |
| mean anomaly at epoch: | 180.0724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|