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 23030.89865062 -.00000050 00000-0 34170-3 0 9997
2 00051 47.2109 265.3144 0107509 128.4634 232.5858 12.18291936780815
| Epoch (UTC): | 30 January 2023 21:34:03 |
| Eccentricity: | 0.0107509 |
| inclination: | 47.2109° |
| perigee height: | 1514 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 265.3144° |
| argument of perigee: | 128.4634° |
| revolutions per day: | 12.18291936 |
| mean anomaly at epoch: | 232.5858° |
| orbit number at epoch: | 78081 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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