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 23332.55026960 .00000749 00000-0 19168-3 0 9998
2 00047 66.6671 26.6959 0217365 102.1637 260.3907 14.43175934316262
| Epoch (UTC): | 28 November 2023 13:12:23 |
| Eccentricity: | 0.0217365 |
| inclination: | 66.6671° |
| perigee height: | 593 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 26.6959° |
| argument of perigee: | 102.1637° |
| revolutions per day: | 14.43175934 |
| mean anomaly at epoch: | 260.3907° |
| orbit number at epoch: | 31626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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