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 43760U 18099C 24340.97643840 .22687725 25922-5 37698-3 0 9991
2 43760 97.4552 54.3313 0009931 279.3000 200.1657 16.47590242329764
Epoch (UTC): | 05 December 2024 23:26:04 |
Eccentricity: | 0.0009931 |
inclination: | 97.4552° |
perigee height: | 139 km |
apogee height: | 152 km |
right ascension of ascending node: | 54.3313° |
argument of perigee: | 279.3000° |
revolutions per day: | 16.47590242 |
mean anomaly at epoch: | 200.1657° |
orbit number at epoch: | 32976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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