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 47U 60007C 23029.22681187 .00000512 00000-0 13636-3 0 9995
2 47 66.6657 118.8148 0231146 322.4604 36.0548 14.42577959272941
| Epoch (UTC): | 29 January 2023 05:26:36 |
| Eccentricity: | 0.0231146 |
| inclination: | 66.6657° |
| perigee height: | 585 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 118.8148° |
| argument of perigee: | 322.4604° |
| revolutions per day: | 14.42577959 |
| mean anomaly at epoch: | 36.0548° |
| orbit number at epoch: | 27294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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