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 42777U 17036N 23083.65307625 .00191995 00000-0 26986-2 0 9991
2 42777 97.1587 128.2851 0004181 35.1510 325.0020 15.56019326320265
Epoch (UTC): | 24 March 2023 15:40:25 |
Eccentricity: | 0.0004181 |
inclination: | 97.1587° |
perigee height: | 396 km |
apogee height: | 402 km |
right ascension of ascending node: | 128.2851° |
argument of perigee: | 35.1510° |
revolutions per day: | 15.56019326 |
mean anomaly at epoch: | 325.0020° |
orbit number at epoch: | 32026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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