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 17526U 87017B 25198.46403126 .00000001 00000-0 -13719-4 0 9992
2 17526 82.9015 353.3584 0039801 344.0982 15.8922 13.77173560912245
Epoch (UTC): | 17 July 2025 11:08:12 |
Eccentricity: | 0.0039801 |
inclination: | 82.9015° |
perigee height: | 944 km |
apogee height: | 1003 km |
right ascension of ascending node: | 353.3584° |
argument of perigee: | 344.0982° |
revolutions per day: | 13.77173560 |
mean anomaly at epoch: | 15.8922° |
orbit number at epoch: | 91224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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