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 42778U 17036P 23080.85145615 .00023811 00000-0 71011-3 0 9991
2 42778 97.1691 117.9489 0010292 66.7363 293.4963 15.34595888319316
Epoch (UTC): | 21 March 2023 20:26:05 |
Eccentricity: | 0.0010292 |
inclination: | 97.1691° |
perigee height: | 455 km |
apogee height: | 469 km |
right ascension of ascending node: | 117.9489° |
argument of perigee: | 66.7363° |
revolutions per day: | 15.34595888 |
mean anomaly at epoch: | 293.4963° |
orbit number at epoch: | 31931 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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