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 35671U 93036APN 24356.53170956 .00001259 00000-0 34658-3 0 9995
2 35671 74.0185 26.7764 0042606 286.6440 224.4331 14.47475246816074
Epoch (UTC): | 21 December 2024 12:45:39 |
Eccentricity: | 0.0042606 |
inclination: | 74.0185° |
perigee height: | 703 km |
apogee height: | 764 km |
right ascension of ascending node: | 26.7764° |
argument of perigee: | 286.6440° |
revolutions per day: | 14.47475246 |
mean anomaly at epoch: | 224.4331° |
orbit number at epoch: | 81607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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