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 00051U 60009C 21016.49968163 -.00000125 00000-0 -37447-3 0 9995
2 00051 47.2143 48.3083 0104270 76.9161 284.3241 12.18270810690064
Epoch (UTC): | 16 January 2021 11:59:32 |
Eccentricity: | 0.0104270 |
inclination: | 47.2143° |
perigee height: | 1517 km |
apogee height: | 1683 km |
right ascension of ascending node: | 48.3083° |
argument of perigee: | 76.9161° |
revolutions per day: | 12.18270810 |
mean anomaly at epoch: | 284.3241° |
orbit number at epoch: | 69006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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