View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16369U 85116B 23331.72471530 .00000143 00000-0 12915-3 0 9996
2 16369 82.9396 37.0937 0037277 51.2714 65.3056 13.76986735905687
| Epoch (UTC): | 27 November 2023 17:23:35 |
| Eccentricity: | 0.0037277 |
| inclination: | 82.9396° |
| perigee height: | 947 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 37.0937° |
| argument of perigee: | 51.2714° |
| revolutions per day: | 13.76986735 |
| mean anomaly at epoch: | 65.3056° |
| orbit number at epoch: | 90568 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|