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 42017U 17008BX 23147.70758412 .00146437 00000-0 10730-2 0 9999
2 42017 97.2096 218.2331 0003185 173.6071 186.5235 15.72725150350240
Epoch (UTC): | 27 May 2023 16:58:55 |
Eccentricity: | 0.0003185 |
inclination: | 97.2096° |
perigee height: | 349 km |
apogee height: | 353 km |
right ascension of ascending node: | 218.2331° |
argument of perigee: | 173.6071° |
revolutions per day: | 15.72725150 |
mean anomaly at epoch: | 186.5235° |
orbit number at epoch: | 35024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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