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 14033U 83037B 24284.30350282 .00002277 00000-0 26203-3 0 9999
2 14033 82.5100 357.2788 0015901 300.6127 59.3520 14.85289617875919
Epoch (UTC): | 10 October 2024 07:17:02 |
Eccentricity: | 0.0015901 |
inclination: | 82.5100° |
perigee height: | 601 km |
apogee height: | 624 km |
right ascension of ascending node: | 357.2788° |
argument of perigee: | 300.6127° |
revolutions per day: | 14.85289617 |
mean anomaly at epoch: | 59.3520° |
orbit number at epoch: | 87591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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