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 00011U 59001A 23342.34102916 .00000573 00000-0 28385-3 0 9991
2 00011 32.8767 327.1152 1460306 221.1768 126.9133 11.87425349425690
| Epoch (UTC): | 08 December 2023 08:11:04 |
| Eccentricity: | 0.1460306 |
| inclination: | 32.8767° |
| perigee height: | 552 km |
| apogee height: | 2923 km |
| right ascension of ascending node: | 327.1152° |
| argument of perigee: | 221.1768° |
| revolutions per day: | 11.87425349 |
| mean anomaly at epoch: | 126.9133° |
| orbit number at epoch: | 42569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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