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 22187.71364762 -.00000042 00000-0 40254-3 0 9992
2 00051 47.2099 189.3934 0108821 231.6156 127.4817 12.18283932755433
| Epoch (UTC): | 06 July 2022 17:07:39 |
| Eccentricity: | 0.0108821 |
| inclination: | 47.2099° |
| perigee height: | 1513 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 189.3934° |
| argument of perigee: | 231.6156° |
| revolutions per day: | 12.18283932 |
| mean anomaly at epoch: | 127.4817° |
| orbit number at epoch: | 75543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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