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 23317U 94066A 23341.30687526 .00001702 00000-0 17006-3 0 9998
2 23317 82.5381 52.6033 0019839 127.9704 232.3311 14.90758778577510
Epoch (UTC): | 07 December 2023 07:21:54 |
Eccentricity: | 0.0019839 |
inclination: | 82.5381° |
perigee height: | 582 km |
apogee height: | 609 km |
right ascension of ascending node: | 52.6033° |
argument of perigee: | 127.9704° |
revolutions per day: | 14.90758778 |
mean anomaly at epoch: | 232.3311° |
orbit number at epoch: | 57751 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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