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 24310.12921082 .00000607 00000-0 52018-3 0 9998
2 116 66.8092 252.0307 0079220 322.0016 37.5490 13.92138795215200
Epoch (UTC): | 05 November 2024 03:06:03 |
Eccentricity: | 0.0079220 |
inclination: | 66.8092° |
perigee height: | 863 km |
apogee height: | 979 km |
right ascension of ascending node: | 252.0307° |
argument of perigee: | 322.0016° |
revolutions per day: | 13.92138795 |
mean anomaly at epoch: | 37.5490° |
orbit number at epoch: | 21520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|