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 12645U 81075A 24357.59850478 .00000274 00000-0 12355-3 0 9998
2 12645 81.2175 23.7182 0062263 323.9792 35.7194 14.18803852243245
Epoch (UTC): | 22 December 2024 14:21:50 |
Eccentricity: | 0.0062263 |
inclination: | 81.2175° |
perigee height: | 784 km |
apogee height: | 874 km |
right ascension of ascending node: | 23.7182° |
argument of perigee: | 323.9792° |
revolutions per day: | 14.18803852 |
mean anomaly at epoch: | 35.7194° |
orbit number at epoch: | 24324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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