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 24283.18254749 .00027951 00000-0 16201-2 0 9998
2 43017 97.5552 154.7655 0197933 271.6201 86.2359 14.97054919372693
| Epoch (UTC): | 09 October 2024 04:22:52 |
| Eccentricity: | 0.0197933 |
| inclination: | 97.5552° |
| perigee height: | 438 km |
| apogee height: | 713 km |
| right ascension of ascending node: | 154.7655° |
| argument of perigee: | 271.6201° |
| revolutions per day: | 14.97054919 |
| mean anomaly at epoch: | 86.2359° |
| orbit number at epoch: | 37269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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