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 13271U 82059A 23275.86874891 .00020248 00000-0 57576-3 0 9997
2 13271 82.4590 59.8840 0005509 138.5863 221.5799 15.36009164259928
Epoch (UTC): | 02 October 2023 20:50:59 |
Eccentricity: | 0.0005509 |
inclination: | 82.4590° |
perigee height: | 454 km |
apogee height: | 461 km |
right ascension of ascending node: | 59.8840° |
argument of perigee: | 138.5863° |
revolutions per day: | 15.36009164 |
mean anomaly at epoch: | 221.5799° |
orbit number at epoch: | 25992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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