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 23335.53022709 .00000723 00000-0 18600-3 0 9998
2 00047 66.6669 18.7149 0217210 99.8892 262.6807 14.43181359316695
| Epoch (UTC): | 01 December 2023 12:43:31 |
| Eccentricity: | 0.0217210 |
| inclination: | 66.6669° |
| perigee height: | 593 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 18.7149° |
| argument of perigee: | 99.8892° |
| revolutions per day: | 14.43181359 |
| mean anomaly at epoch: | 262.6807° |
| orbit number at epoch: | 31669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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