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 23267.12445410 .00002428 00000-0 24698-3 0 9990
2 23317 82.5350 122.7239 0019478 21.5855 338.6180 14.90244545566477
Epoch (UTC): | 24 September 2023 02:59:12 |
Eccentricity: | 0.0019478 |
inclination: | 82.5350° |
perigee height: | 583 km |
apogee height: | 611 km |
right ascension of ascending node: | 122.7239° |
argument of perigee: | 21.5855° |
revolutions per day: | 14.90244545 |
mean anomaly at epoch: | 338.6180° |
orbit number at epoch: | 56647 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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