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 22144.12186162 .00000419 00000-0 47772-4 0 9995
2 17192 82.5076 5.0681 0015484 282.6536 197.2364 14.83765023915842
Epoch (UTC): | 24 May 2022 02:55:28 |
Eccentricity: | 0.0015484 |
inclination: | 82.5076° |
perigee height: | 606 km |
apogee height: | 628 km |
right ascension of ascending node: | 5.0681° |
argument of perigee: | 282.6536° |
revolutions per day: | 14.83765023 |
mean anomaly at epoch: | 197.2364° |
orbit number at epoch: | 91584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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