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 43017U 17073E 24278.36967856 .00028110 00000-0 16346-2 0 9990
2 43017 97.5560 150.1096 0199112 287.9956 69.9656 14.96786001371970
| Epoch (UTC): | 04 October 2024 08:52:20 |
| Eccentricity: | 0.0199112 |
| inclination: | 97.5560° |
| perigee height: | 438 km |
| apogee height: | 715 km |
| right ascension of ascending node: | 150.1096° |
| argument of perigee: | 287.9956° |
| revolutions per day: | 14.96786001 |
| mean anomaly at epoch: | 69.9656° |
| orbit number at epoch: | 37197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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