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 00050U 60009B 21023.79232386 -.00000113 00000-0 -26872-3 0 9993
2 00050 47.2304 157.4124 0113581 262.1292 96.6592 12.20114523697127
Epoch (UTC): | 23 January 2021 19:00:56 |
Eccentricity: | 0.0113581 |
inclination: | 47.2304° |
perigee height: | 1501 km |
apogee height: | 1682 km |
right ascension of ascending node: | 157.4124° |
argument of perigee: | 262.1292° |
revolutions per day: | 12.20114523 |
mean anomaly at epoch: | 96.6592° |
orbit number at epoch: | 69712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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