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 14781U 84021B 22141.54182463 .00001573 00000-0 19654-3 0 9993
2 14781 97.6162 130.2052 0009756 56.8660 303.3490 14.83632239 36052
Epoch (UTC): | 21 May 2022 13:00:13 |
Eccentricity: | 0.0009756 |
inclination: | 97.6162° |
perigee height: | 611 km |
apogee height: | 625 km |
right ascension of ascending node: | 130.2052° |
argument of perigee: | 56.8660° |
revolutions per day: | 14.83632239 |
mean anomaly at epoch: | 303.3490° |
orbit number at epoch: | 3605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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