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 22178.93090685 .00010061 00000-0 29904-3 0 9995
2 42017 97.2688 244.8938 0005053 186.4715 173.6464 15.34939039298689
Epoch (UTC): | 27 June 2022 22:20:30 |
Eccentricity: | 0.0005053 |
inclination: | 97.2688° |
perigee height: | 457 km |
apogee height: | 464 km |
right ascension of ascending node: | 244.8938° |
argument of perigee: | 186.4715° |
revolutions per day: | 15.34939039 |
mean anomaly at epoch: | 173.6464° |
orbit number at epoch: | 29868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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