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 34814U 93036ABD 24357.76276257 .00003961 00000-0 13872-2 0 9996
2 34814 73.8967 262.5683 0058659 223.8431 169.0419 14.34473131823183
Epoch (UTC): | 22 December 2024 18:18:22 |
Eccentricity: | 0.0058659 |
inclination: | 73.8967° |
perigee height: | 735 km |
apogee height: | 819 km |
right ascension of ascending node: | 262.5683° |
argument of perigee: | 223.8431° |
revolutions per day: | 14.34473131 |
mean anomaly at epoch: | 169.0419° |
orbit number at epoch: | 82318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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