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 23150.44050423 .00000495 00000-0 55908-4 0 9993
2 15370 82.5143 129.7094 0022402 86.3351 274.0426 14.84264655 86430
Epoch (UTC): | 30 May 2023 10:34:19 |
Eccentricity: | 0.0022402 |
inclination: | 82.5143° |
perigee height: | 600 km |
apogee height: | 631 km |
right ascension of ascending node: | 129.7094° |
argument of perigee: | 86.3351° |
revolutions per day: | 14.84264655 |
mean anomaly at epoch: | 274.0426° |
orbit number at epoch: | 8643 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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