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 21022.80947894 -.00000099 00000-0 -13901-3 0 9993
2 00050 47.2301 160.4628 0113566 259.2083 99.5905 12.20114580697005
Epoch (UTC): | 22 January 2021 19:25:38 |
Eccentricity: | 0.0113566 |
inclination: | 47.2301° |
perigee height: | 1501 km |
apogee height: | 1682 km |
right ascension of ascending node: | 160.4628° |
argument of perigee: | 259.2083° |
revolutions per day: | 12.20114580 |
mean anomaly at epoch: | 99.5905° |
orbit number at epoch: | 69700 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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