View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20401U 90001A 23334.81775000 -.00000252 00000-0 00000+0 0 9999
2 20401 12.8474 354.9442 0012224 284.6484 61.0384 0.99000515119678
Epoch (UTC): | 30 November 2023 19:37:33 |
Eccentricity: | 0.0012224 |
inclination: | 12.8474° |
perigee height: | 36094 km |
apogee height: | 36198 km |
right ascension of ascending node: | 354.9442° |
argument of perigee: | 284.6484° |
revolutions per day: | 0.99000515 |
mean anomaly at epoch: | 61.0384° |
orbit number at epoch: | 11967 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|