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 25345.31759074 .00000263 00000-0 99205-4 0 9992
2 27386 98.3597 296.0941 0001139 82.1759 37.7057 14.38998533246460
| Epoch (UTC): | 11 December 2025 07:37:19 |
| Eccentricity: | 0.0001139 |
| inclination: | 98.3597° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 296.0941° |
| argument of perigee: | 82.1759° |
| revolutions per day: | 14.38998533 |
| mean anomaly at epoch: | 37.7057° |
| orbit number at epoch: | 24646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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