View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 4332U 70012B 23341.53614858 .00000222 00000-0 99824-4 0 9997
2 4332 98.9395 214.4064 0060169 357.8003 2.2905 14.31217780803234
Epoch (UTC): | 07 December 2023 12:52:03 |
Eccentricity: | 0.0060169 |
inclination: | 98.9395° |
perigee height: | 744 km |
apogee height: | 831 km |
right ascension of ascending node: | 214.4064° |
argument of perigee: | 357.8003° |
revolutions per day: | 14.31217780 |
mean anomaly at epoch: | 2.2905° |
orbit number at epoch: | 80323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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