View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39059U 13001C 23083.75695675 .00000044 00000-0 24555-3 0 9999
2 39059 82.4997 235.8198 0027056 89.6729 270.7447 12.42874281462129
Epoch (UTC): | 24 March 2023 18:10:01 |
Eccentricity: | 0.0027056 |
inclination: | 82.4997° |
perigee height: | 1473 km |
apogee height: | 1516 km |
right ascension of ascending node: | 235.8198° |
argument of perigee: | 89.6729° |
revolutions per day: | 12.42874281 |
mean anomaly at epoch: | 270.7447° |
orbit number at epoch: | 46212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|