View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16682U 86030B 23340.14232932 .00000346 00000-0 12690-3 0 9992
2 16682 74.0245 205.9521 0015086 326.9408 151.8308 14.36426536970049
Epoch (UTC): | 06 December 2023 03:24:57 |
Eccentricity: | 0.0015086 |
inclination: | 74.0245° |
perigee height: | 759 km |
apogee height: | 781 km |
right ascension of ascending node: | 205.9521° |
argument of perigee: | 326.9408° |
revolutions per day: | 14.36426536 |
mean anomaly at epoch: | 151.8308° |
orbit number at epoch: | 97004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|