View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 3214U 68012D 24334.34722685 .00000338 00000-0 64746-3 0 9994
2 3214 89.8429 112.9606 0187044 33.2013 355.8731 13.29061783745988
Epoch (UTC): | 29 November 2024 08:20:00 |
Eccentricity: | 0.0187044 |
inclination: | 89.8429° |
perigee height: | 1009 km |
apogee height: | 1291 km |
right ascension of ascending node: | 112.9606° |
argument of perigee: | 33.2013° |
revolutions per day: | 13.29061783 |
mean anomaly at epoch: | 355.8731° |
orbit number at epoch: | 74598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|