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 25340.85479697 .00000287 00000-0 10679-3 0 9999
2 27386 98.3591 291.7448 0001140 81.9869 332.2777 14.38995949245828
| Epoch (UTC): | 06 December 2025 20:30:54 |
| Eccentricity: | 0.0001140 |
| inclination: | 98.3591° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 291.7448° |
| argument of perigee: | 81.9869° |
| revolutions per day: | 14.38995949 |
| mean anomaly at epoch: | 332.2777° |
| orbit number at epoch: | 24582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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