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 54920U 22151RH 24358.06749008 .00022466 00000-0 45558-2 0 9996
2 54920 98.6665 30.1644 0094101 148.7316 211.9526 14.58411807107806
Epoch (UTC): | 23 December 2024 01:37:11 |
Eccentricity: | 0.0094101 |
inclination: | 98.6665° |
perigee height: | 632 km |
apogee height: | 765 km |
right ascension of ascending node: | 30.1644° |
argument of perigee: | 148.7316° |
revolutions per day: | 14.58411807 |
mean anomaly at epoch: | 211.9526° |
orbit number at epoch: | 10780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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