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 18957U 88019A 24282.71851189 .00000098 00000-0 17795-3 0 9993
2 18957 65.0432 276.2198 0029389 76.9968 283.4369 13.79769144844094
Epoch (UTC): | 08 October 2024 17:14:39 |
Eccentricity: | 0.0029389 |
inclination: | 65.0432° |
perigee height: | 943 km |
apogee height: | 986 km |
right ascension of ascending node: | 276.2198° |
argument of perigee: | 76.9968° |
revolutions per day: | 13.79769144 |
mean anomaly at epoch: | 283.4369° |
orbit number at epoch: | 84409 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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