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 14760U 84019B 22140.52492190 .00000335 00000-0 12396-3 0 9996
2 14760 74.0452 62.6020 0028383 202.5502 157.4406 14.35978137 1699
Epoch (UTC): | 20 May 2022 12:35:53 |
Eccentricity: | 0.0028383 |
inclination: | 74.0452° |
perigee height: | 751 km |
apogee height: | 792 km |
right ascension of ascending node: | 62.6020° |
argument of perigee: | 202.5502° |
revolutions per day: | 14.35978137 |
mean anomaly at epoch: | 157.4406° |
orbit number at epoch: | 169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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