View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39483U 13076A 23084.10700044 .00000010 00000-0 -20353-5 0 9997
2 39483 82.4891 184.1060 0020349 145.5849 214.6557 12.42894585419490
Epoch (UTC): | 25 March 2023 02:34:04 |
Eccentricity: | 0.0020349 |
inclination: | 82.4891° |
perigee height: | 1478 km |
apogee height: | 1510 km |
right ascension of ascending node: | 184.1060° |
argument of perigee: | 145.5849° |
revolutions per day: | 12.42894585 |
mean anomaly at epoch: | 214.6557° |
orbit number at epoch: | 41949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|