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 21062.84505340 -.00000021 00000-0 60850-3 0 9997
2 00051 47.2110 264.9310 0105183 213.6509 145.7568 12.18272679695711
Epoch (UTC): | 03 March 2021 20:16:52 |
Eccentricity: | 0.0105183 |
inclination: | 47.2110° |
perigee height: | 1516 km |
apogee height: | 1684 km |
right ascension of ascending node: | 264.9310° |
argument of perigee: | 213.6509° |
revolutions per day: | 12.18272679 |
mean anomaly at epoch: | 145.7568° |
orbit number at epoch: | 69571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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