View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16494U 86005B 25318.45682617 .00000234 00000-0 22256-3 0 9990
2 16494 82.9290 306.3773 0018097 287.6771 182.8239 13.76761798 343
| Epoch (UTC): | 14 November 2025 10:57:49 |
| Eccentricity: | 0.0018097 |
| inclination: | 82.9290° |
| perigee height: | 962 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 306.3773° |
| argument of perigee: | 287.6771° |
| revolutions per day: | 13.76761798 |
| mean anomaly at epoch: | 182.8239° |
| orbit number at epoch: | 34 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|