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 15370U 84111B 23152.39553924 .00000540 00000-0 61322-4 0 9991
2 15370 82.5145 127.8746 0022381 80.3625 280.0118 14.84266853 65624
Epoch (UTC): | 01 June 2023 09:29:34 |
Eccentricity: | 0.0022381 |
inclination: | 82.5145° |
perigee height: | 600 km |
apogee height: | 631 km |
right ascension of ascending node: | 127.8746° |
argument of perigee: | 80.3625° |
revolutions per day: | 14.84266853 |
mean anomaly at epoch: | 280.0118° |
orbit number at epoch: | 6562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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