View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00016U 58002A 23337.47763725 .00000827 00000-0 11652-2 0 9995
2 00016 34.2600 104.4935 2020562 167.9854 197.7384 10.48988585591557
Epoch (UTC): | 03 December 2023 11:27:47 |
Eccentricity: | 0.2020562 |
inclination: | 34.2600° |
perigee height: | 656 km |
apogee height: | 4218 km |
right ascension of ascending node: | 104.4935° |
argument of perigee: | 167.9854° |
revolutions per day: | 10.48988585 |
mean anomaly at epoch: | 197.7384° |
orbit number at epoch: | 59155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|