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 26017.84606897 +.00000000 +00000-0 +38302-4 0 00003
2 27386 98.3649 332.6810 0001155 91.8309 288.8463 14.39014007 00
| Epoch (UTC): | 17 January 2026 20:18:20 |
| Eccentricity: | 0.0001155 |
| inclination: | 98.3649° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 332.6810° |
| argument of perigee: | 91.8309° |
| revolutions per day: | 14.39014007 |
| mean anomaly at epoch: | 288.8463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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