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 17192U 86097B 22139.13051196 .00000498 00000-0 57198-4 0 9998
2 17192 82.5081 9.7550 0015572 300.4458 174.3769 14.83761042915105
Epoch (UTC): | 19 May 2022 03:07:56 |
Eccentricity: | 0.0015572 |
inclination: | 82.5081° |
perigee height: | 606 km |
apogee height: | 628 km |
right ascension of ascending node: | 9.7550° |
argument of perigee: | 300.4458° |
revolutions per day: | 14.83761042 |
mean anomaly at epoch: | 174.3769° |
orbit number at epoch: | 91510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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