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 23030.07839248 -.00000059 00000-0 26097-3 0 9992
2 00051 47.2110 267.8523 0107466 126.0230 235.0573 12.18291904780719
| Epoch (UTC): | 30 January 2023 01:52:53 |
| Eccentricity: | 0.0107466 |
| inclination: | 47.2110° |
| perigee height: | 1514 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 267.8523° |
| argument of perigee: | 126.0230° |
| revolutions per day: | 12.18291904 |
| mean anomaly at epoch: | 235.0573° |
| orbit number at epoch: | 78071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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