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 23339.13388101 .00000491 00000-0 13413-3 0 9998
2 47 66.6665 9.0630 0217148 97.1440 265.4408 14.43186512317650
| Epoch (UTC): | 05 December 2023 03:12:47 |
| Eccentricity: | 0.0217148 |
| inclination: | 66.6665° |
| perigee height: | 593 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 9.0630° |
| argument of perigee: | 97.1440° |
| revolutions per day: | 14.43186512 |
| mean anomaly at epoch: | 265.4408° |
| orbit number at epoch: | 31765 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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