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 24258.63466463 .00009713 00000-0 10525-2 0 9991
2 37224 71.9706 86.3322 0016805 209.9453 150.0755 14.88278055 21134
Epoch (UTC): | 14 September 2024 15:13:55 |
Eccentricity: | 0.0016805 |
inclination: | 71.9706° |
perigee height: | 591 km |
apogee height: | 615 km |
right ascension of ascending node: | 86.3322° |
argument of perigee: | 209.9453° |
revolutions per day: | 14.88278055 |
mean anomaly at epoch: | 150.0755° |
orbit number at epoch: | 2113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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