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 37162U 10046A 24301.20358907 0.00000000 00000-0 00000-0 0 07
2 37162 122.9901 240.5357 0005797 125.1274 234.8726 13.41445942 00
Epoch (UTC): | 27 October 2024 04:53:10 |
Eccentricity: | 0.0005797 |
inclination: | 122.9901° |
perigee height: | 1099 km |
apogee height: | 1108 km |
right ascension of ascending node: | 240.5357° |
argument of perigee: | 125.1274° |
revolutions per day: | 13.41445942 |
mean anomaly at epoch: | 234.8726° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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