View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29165U 06020D 24277.28823635 .00000247 00000-0 57637-3 0 9994
2 29165 6.8334 357.8803 5507212 122.5544 302.5515 4.56548724216878
Epoch (UTC): | 03 October 2024 06:55:03 |
Eccentricity: | 0.5507212 |
inclination: | 6.8334° |
perigee height: | 518 km |
apogee height: | 17423 km |
right ascension of ascending node: | 357.8803° |
argument of perigee: | 122.5544° |
revolutions per day: | 4.56548724 |
mean anomaly at epoch: | 302.5515° |
orbit number at epoch: | 21687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|