View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27534U 02046A 23083.61514377 .00000076 00000-0 66208-4 0 9992
2 27534 82.9326 123.1021 0036582 16.0671 95.6995 13.72784035 26571
Epoch (UTC): | 24 March 2023 14:45:48 |
Eccentricity: | 0.0036582 |
inclination: | 82.9326° |
perigee height: | 962 km |
apogee height: | 1016 km |
right ascension of ascending node: | 123.1021° |
argument of perigee: | 16.0671° |
revolutions per day: | 13.72784035 |
mean anomaly at epoch: | 95.6995° |
orbit number at epoch: | 2657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|