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 23087.24559490 .00099079 00000-0 13897-2 0 9992
2 42017 97.2229 156.4094 0002485 269.1328 90.9643 15.56408743340793
Epoch (UTC): | 28 March 2023 05:53:39 |
Eccentricity: | 0.0002485 |
inclination: | 97.2229° |
perigee height: | 396 km |
apogee height: | 400 km |
right ascension of ascending node: | 156.4094° |
argument of perigee: | 269.1328° |
revolutions per day: | 15.56408743 |
mean anomaly at epoch: | 90.9643° |
orbit number at epoch: | 34079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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