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 40074U 14037F 24357.87336294 .00016641 00000-0 13363-2 0 9999
2 40074 98.3645 300.3640 0003186 105.2360 254.9214 15.00133966567002
Epoch (UTC): | 22 December 2024 20:57:38 |
Eccentricity: | 0.0003186 |
inclination: | 98.3645° |
perigee height: | 564 km |
apogee height: | 569 km |
right ascension of ascending node: | 300.3640° |
argument of perigee: | 105.2360° |
revolutions per day: | 15.00133966 |
mean anomaly at epoch: | 254.9214° |
orbit number at epoch: | 56700 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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