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 1807U 65098C 24256.89285120 .00002506 00000-0 83931-3 0 9998
2 1807 79.8361 225.2634 1335901 252.8986 92.1829 12.26709328594119
Epoch (UTC): | 12 September 2024 21:25:42 |
Eccentricity: | 0.1335901 |
inclination: | 79.8361° |
perigee height: | 502 km |
apogee height: | 2624 km |
right ascension of ascending node: | 225.2634° |
argument of perigee: | 252.8986° |
revolutions per day: | 12.26709328 |
mean anomaly at epoch: | 92.1829° |
orbit number at epoch: | 59411 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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