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 23657U 95046A 23336.88175575 .00002782 00000-0 29319-3 0 9996
2 23657 82.5267 201.8705 0020557 178.8851 181.2417 14.88859663527719
Epoch (UTC): | 02 December 2023 21:09:43 |
Eccentricity: | 0.0020557 |
inclination: | 82.5267° |
perigee height: | 587 km |
apogee height: | 616 km |
right ascension of ascending node: | 201.8705° |
argument of perigee: | 178.8851° |
revolutions per day: | 14.88859663 |
mean anomaly at epoch: | 181.2417° |
orbit number at epoch: | 52771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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