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 37224U 10062C 24260.78554969 .00007346 00000-0 79751-3 0 9996
2 37224 71.9703 81.5010 0016676 206.1427 153.8901 14.88302608 21459
Epoch (UTC): | 16 September 2024 18:51:11 |
Eccentricity: | 0.0016676 |
inclination: | 71.9703° |
perigee height: | 591 km |
apogee height: | 615 km |
right ascension of ascending node: | 81.5010° |
argument of perigee: | 206.1427° |
revolutions per day: | 14.88302608 |
mean anomaly at epoch: | 153.8901° |
orbit number at epoch: | 2145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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