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 24297U 96051A 24358.24553425 -.00000149 00000-0 -53479-4 0 9995
2 24297 70.9044 34.0629 0021937 40.0749 320.1985 14.13682756460157
Epoch (UTC): | 23 December 2024 05:53:34 |
Eccentricity: | 0.0021937 |
inclination: | 70.9044° |
perigee height: | 831 km |
apogee height: | 862 km |
right ascension of ascending node: | 34.0629° |
argument of perigee: | 40.0749° |
revolutions per day: | 14.13682756 |
mean anomaly at epoch: | 320.1985° |
orbit number at epoch: | 46015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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