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 22224.77451072 .00000236 00000-0 25431-4 0 9996
2 15370 82.5150 42.3845 0019952 329.0439 30.9598 14.83918456 22222
Epoch (UTC): | 12 August 2022 18:35:17 |
Eccentricity: | 0.0019952 |
inclination: | 82.5150° |
perigee height: | 603 km |
apogee height: | 631 km |
right ascension of ascending node: | 42.3845° |
argument of perigee: | 329.0439° |
revolutions per day: | 14.83918456 |
mean anomaly at epoch: | 30.9598° |
orbit number at epoch: | 2222 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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