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 27939U 03042A 23080.13527307 .00002060 00000-0 36707-3 0 9994
2 27939 98.2256 226.5217 0013286 58.5537 301.6952 14.68074177 41626
Epoch (UTC): | 21 March 2023 03:14:47 |
Eccentricity: | 0.0013286 |
inclination: | 98.2256° |
perigee height: | 658 km |
apogee height: | 676 km |
right ascension of ascending node: | 226.5217° |
argument of perigee: | 58.5537° |
revolutions per day: | 14.68074177 |
mean anomaly at epoch: | 301.6952° |
orbit number at epoch: | 4162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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