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 54283U 22151AA 24315.21934999 .00001264 00000-0 75242-3 0 9990
2 54283 98.8062 311.6150 0052461 198.4051 161.5221 14.08499144102072
Epoch (UTC): | 10 November 2024 05:15:51 |
Eccentricity: | 0.0052461 |
inclination: | 98.8062° |
perigee height: | 826 km |
apogee height: | 902 km |
right ascension of ascending node: | 311.6150° |
argument of perigee: | 198.4051° |
revolutions per day: | 14.08499144 |
mean anomaly at epoch: | 161.5221° |
orbit number at epoch: | 10207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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