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 37855U 11061F 23344.78015699 .00030521 00000-0 67321-3 0 9991
2 37855 101.6968 48.0893 0092681 214.9800 144.5319 15.39375230664071
Epoch (UTC): | 10 December 2023 18:43:25 |
Eccentricity: | 0.0092681 |
inclination: | 101.6968° |
perigee height: | 384 km |
apogee height: | 511 km |
right ascension of ascending node: | 48.0893° |
argument of perigee: | 214.9800° |
revolutions per day: | 15.39375230 |
mean anomaly at epoch: | 144.5319° |
orbit number at epoch: | 66407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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