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 35744U 97051RX 24358.13712189 .00013020 00000-0 24501-2 0 9999
2 35744 86.3320 124.8263 0024519 341.2969 18.7339 14.64326832822460
Epoch (UTC): | 23 December 2024 03:17:27 |
Eccentricity: | 0.0024519 |
inclination: | 86.3320° |
perigee height: | 662 km |
apogee height: | 696 km |
right ascension of ascending node: | 124.8263° |
argument of perigee: | 341.2969° |
revolutions per day: | 14.64326832 |
mean anomaly at epoch: | 18.7339° |
orbit number at epoch: | 82246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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