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 15595U 85021A 19345.48842094 -.00000085 +00000-0 +16695-4 0 9997
2 15595 108.0348 177.4776 0002603 264.9457 095.1387 14.38135473820550
Epoch (UTC): | 11 December 2019 11:43:19 |
Eccentricity: | 0.0002603 |
inclination: | 108.0348° |
perigee height: | 763 km |
apogee height: | 766 km |
right ascension of ascending node: | 177.4776° |
argument of perigee: | 264.9457° |
revolutions per day: | 14.38135473 |
mean anomaly at epoch: | 95.1387° |
orbit number at epoch: | 82055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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