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 25544U 98067A 24307.19144382 .00029067 00000-0 49703-3 0 9998
2 25544 51.6394 351.7794 0008989 127.7251 232.4555 15.50990788479957
Epoch (UTC): | 02 November 2024 04:35:40 |
Eccentricity: | 0.0008989 |
inclination: | 51.6394° |
perigee height: | 408 km |
apogee height: | 420 km |
right ascension of ascending node: | 351.7794° |
argument of perigee: | 127.7251° |
revolutions per day: | 15.50990788 |
mean anomaly at epoch: | 232.4555° |
orbit number at epoch: | 47995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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