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 43678U 18084H 24262.80651842 .00004445 00000-0 40122-3 0 9998
2 43678 98.0834 63.6393 0010340 83.0391 277.2005 14.96011547320910
| Epoch (UTC): | 18 September 2024 19:21:23 |
| Eccentricity: | 0.0010340 |
| inclination: | 98.0834° |
| perigee height: | 572 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 63.6393° |
| argument of perigee: | 83.0391° |
| revolutions per day: | 14.96011547 |
| mean anomaly at epoch: | 277.2005° |
| orbit number at epoch: | 32091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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