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 31087U 99025BGH 24357.53535174 .00008404 00000-0 15283-2 0 9995
2 31087 98.1321 20.0106 0183694 319.1874 199.0504 14.55985903936036
Epoch (UTC): | 22 December 2024 12:50:54 |
Eccentricity: | 0.0183694 |
inclination: | 98.1321° |
perigee height: | 576 km |
apogee height: | 836 km |
right ascension of ascending node: | 20.0106° |
argument of perigee: | 319.1874° |
revolutions per day: | 14.55985903 |
mean anomaly at epoch: | 199.0504° |
orbit number at epoch: | 93603 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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