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 22176.12760757 .00011557 00000-0 34394-3 0 9998
2 42017 97.2690 242.1304 0004752 196.2406 163.8686 15.34862401298259
Epoch (UTC): | 25 June 2022 03:03:45 |
Eccentricity: | 0.0004752 |
inclination: | 97.2690° |
perigee height: | 458 km |
apogee height: | 464 km |
right ascension of ascending node: | 242.1304° |
argument of perigee: | 196.2406° |
revolutions per day: | 15.34862401 |
mean anomaly at epoch: | 163.8686° |
orbit number at epoch: | 29825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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