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 37851U 11061B 23272.58286498 .00040187 00000-0 11557-2 0 9990
2 37851 101.7312 283.4783 0115674 122.3932 238.8548 15.29207619651947
Epoch (UTC): | 29 September 2023 13:59:19 |
Eccentricity: | 0.0115674 |
inclination: | 101.7312° |
perigee height: | 399 km |
apogee height: | 557 km |
right ascension of ascending node: | 283.4783° |
argument of perigee: | 122.3932° |
revolutions per day: | 15.29207619 |
mean anomaly at epoch: | 238.8548° |
orbit number at epoch: | 65194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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