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 25197.88662774 .00000381 00000-0 41099-4 0 9991
2 17192 82.5063 4.2493 0017858 85.4987 27.7894 14.85605118 65331
Epoch (UTC): | 16 July 2025 21:16:44 |
Eccentricity: | 0.0017858 |
inclination: | 82.5063° |
perigee height: | 599 km |
apogee height: | 624 km |
right ascension of ascending node: | 4.2493° |
argument of perigee: | 85.4987° |
revolutions per day: | 14.85605118 |
mean anomaly at epoch: | 27.7894° |
orbit number at epoch: | 6533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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