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 27386U 02009A 24260.12649396 .00000722 00000-0 24909-3 0 9999
2 27386 98.2925 218.0984 0001258 89.7880 280.6982 14.38675605181652
| Epoch (UTC): | 16 September 2024 03:02:09 |
| Eccentricity: | 0.0001258 |
| inclination: | 98.2925° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 218.0984° |
| argument of perigee: | 89.7880° |
| revolutions per day: | 14.38675605 |
| mean anomaly at epoch: | 280.6982° |
| orbit number at epoch: | 18165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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