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 17295U 87003A 24311.83051910 .00040941 00000-0 10511-2 0 9998
2 17295 82.5051 351.6379 0003472 102.1788 257.9846 15.39130816 68679
Epoch (UTC): | 06 November 2024 19:55:56 |
Eccentricity: | 0.0003472 |
inclination: | 82.5051° |
perigee height: | 446 km |
apogee height: | 451 km |
right ascension of ascending node: | 351.6379° |
argument of perigee: | 102.1788° |
revolutions per day: | 15.39130816 |
mean anomaly at epoch: | 257.9846° |
orbit number at epoch: | 6867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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