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 24278.50642753 .00001000 00000-0 33985-3 0 9994
2 27386 98.2962 235.8670 0001307 89.5500 20.2233 14.38697758184220
| Epoch (UTC): | 04 October 2024 12:09:15 |
| Eccentricity: | 0.0001307 |
| inclination: | 98.2962° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 235.8670° |
| argument of perigee: | 89.5500° |
| revolutions per day: | 14.38697758 |
| mean anomaly at epoch: | 20.2233° |
| orbit number at epoch: | 18422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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