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 36794U 10034C 24276.75979292 .00004346 00000-0 13054-2 0 9990
2 36794 49.5108 305.6587 5443972 109.5545 315.0507 4.86469231245077
Epoch (UTC): | 02 October 2024 18:14:06 |
Eccentricity: | 0.5443972 |
inclination: | 49.5108° |
perigee height: | 325 km |
apogee height: | 16344 km |
right ascension of ascending node: | 305.6587° |
argument of perigee: | 109.5545° |
revolutions per day: | 4.86469231 |
mean anomaly at epoch: | 315.0507° |
orbit number at epoch: | 24507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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