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 23342.46032118 .00000251 00000-0 80698-4 0 9996
2 00047 66.6663 0.1536 0217130 94.6323 267.9616 14.43189443317696
| Epoch (UTC): | 08 December 2023 11:02:51 |
| Eccentricity: | 0.0217130 |
| inclination: | 66.6663° |
| perigee height: | 593 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 0.1536° |
| argument of perigee: | 94.6323° |
| revolutions per day: | 14.43189443 |
| mean anomaly at epoch: | 267.9616° |
| orbit number at epoch: | 31769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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