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 00047U 60007C 22331.62017380 .00000455 00000-0 12571-3 0 9995
2 00047 66.6655 286.3369 0225576 7.8500 352.6036 14.42488854263476
| Epoch (UTC): | 27 November 2022 14:53:03 |
| Eccentricity: | 0.0225576 |
| inclination: | 66.6655° |
| perigee height: | 589 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 286.3369° |
| argument of perigee: | 7.8500° |
| revolutions per day: | 14.42488854 |
| mean anomaly at epoch: | 352.6036° |
| orbit number at epoch: | 26347 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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