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 27665U 03005C 21016.85142503 .00000043 00000-0 50626-4 0 9992
2 27665 39.5758 281.1678 0008654 151.8981 266.3017 14.28542297938160
Epoch (UTC): | 16 January 2021 20:26:03 |
Eccentricity: | 0.0008654 |
inclination: | 39.5758° |
perigee height: | 790 km |
apogee height: | 803 km |
right ascension of ascending node: | 281.1678° |
argument of perigee: | 151.8981° |
revolutions per day: | 14.28542297 |
mean anomaly at epoch: | 266.3017° |
orbit number at epoch: | 93816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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