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 23036.88652112 .00000019 00000-0 10056-2 0 9992
2 00051 47.2100 246.7875 0107715 146.2957 214.4739 12.18292744781541
| Epoch (UTC): | 05 February 2023 21:16:35 |
| Eccentricity: | 0.0107715 |
| inclination: | 47.2100° |
| perigee height: | 1514 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 246.7875° |
| argument of perigee: | 146.2957° |
| revolutions per day: | 12.18292744 |
| mean anomaly at epoch: | 214.4739° |
| orbit number at epoch: | 78154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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