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 25347.62250859 .00000218 00000-0 84536-4 0 9996
2 27386 98.3601 298.3406 0001132 83.1589 90.1955 14.38999682246794
| Epoch (UTC): | 13 December 2025 14:56:24 |
| Eccentricity: | 0.0001132 |
| inclination: | 98.3601° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 298.3406° |
| argument of perigee: | 83.1589° |
| revolutions per day: | 14.38999682 |
| mean anomaly at epoch: | 90.1955° |
| orbit number at epoch: | 24679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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