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 is defined by the following mean orbital elements,
1 27386U 26018.88791366 +.00000000 +00000-0 +45707-4 0 00001
2 27386 98.3651 333.6970 0001158 91.8955 282.8809 14.39014397 01
| Epoch (UTC): | 18 January 2026 21:18:35 |
| Eccentricity: | 0.0001158 |
| inclination: | 98.3651° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 333.6970° |
| argument of perigee: | 91.8955° |
| revolutions per day: | 14.39014397 |
| mean anomaly at epoch: | 282.8809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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