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 23038.77310567 -.00000014 00000-0 68625-3 0 9999
2 00051 47.2100 240.9504 0107785 151.9144 208.7514 12.18292956781771
| Epoch (UTC): | 07 February 2023 18:33:16 |
| Eccentricity: | 0.0107785 |
| inclination: | 47.2100° |
| perigee height: | 1514 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 240.9504° |
| argument of perigee: | 151.9144° |
| revolutions per day: | 12.18292956 |
| mean anomaly at epoch: | 208.7514° |
| orbit number at epoch: | 78177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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