View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 116U 61015A 23270.84215226 .00000081 00000-0 12082-3 0 9990
2 116 66.8095 160.7786 0082117 251.0569 108.1597 13.91947273158939
Epoch (UTC): | 27 September 2023 20:12:41 |
Eccentricity: | 0.0082117 |
inclination: | 66.8095° |
perigee height: | 862 km |
apogee height: | 982 km |
right ascension of ascending node: | 160.7786° |
argument of perigee: | 251.0569° |
revolutions per day: | 13.91947273 |
mean anomaly at epoch: | 108.1597° |
orbit number at epoch: | 15893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|