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 42759U 17034B 24253.51650687 .00042105 00000-0 13032-2 0 9999
2 42759 43.0152 108.5865 0012607 204.9573 155.0672 15.32714782400328
| Epoch (UTC): | 09 September 2024 12:23:46 |
| Eccentricity: | 0.0012607 |
| inclination: | 43.0152° |
| perigee height: | 459 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.5865° |
| argument of perigee: | 204.9573° |
| revolutions per day: | 15.32714782 |
| mean anomaly at epoch: | 155.0672° |
| orbit number at epoch: | 40032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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