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 21022.73381399 -.00000088 00000-0 -23024-4 0 9994
2 00051 47.2146 29.0219 0104253 95.3242 265.9451 12.18270537690828
Epoch (UTC): | 22 January 2021 17:36:41 |
Eccentricity: | 0.0104253 |
inclination: | 47.2146° |
perigee height: | 1517 km |
apogee height: | 1683 km |
right ascension of ascending node: | 29.0219° |
argument of perigee: | 95.3242° |
revolutions per day: | 12.18270537 |
mean anomaly at epoch: | 265.9451° |
orbit number at epoch: | 69082 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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