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 24282.87717036 .00000791 00000-0 27167-3 0 9997
2 27386 98.2971 240.0935 0001355 90.3656 323.7705 14.38704898184855
| Epoch (UTC): | 08 October 2024 21:03:07 |
| Eccentricity: | 0.0001355 |
| inclination: | 98.2971° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 240.0935° |
| argument of perigee: | 90.3656° |
| revolutions per day: | 14.38704898 |
| mean anomaly at epoch: | 323.7705° |
| orbit number at epoch: | 18485 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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