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 34953U 93036AEG 24357.41298522 .00008438 00000-0 15861-2 0 9995
2 34953 74.0957 350.3649 0060148 78.9788 49.8853 14.63599451829197
Epoch (UTC): | 22 December 2024 09:54:41 |
Eccentricity: | 0.0060148 |
inclination: | 74.0957° |
perigee height: | 639 km |
apogee height: | 724 km |
right ascension of ascending node: | 350.3649° |
argument of perigee: | 78.9788° |
revolutions per day: | 14.63599451 |
mean anomaly at epoch: | 49.8853° |
orbit number at epoch: | 82919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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