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 26158.79335659 +.00000000 +00000-0 +49598-4 0 00007
2 27386 98.3830 110.3215 0001340 91.0170 331.4929 14.39062705 06
| Epoch (UTC): | 07 June 2026 19:02:26 |
| Eccentricity: | 0.0001340 |
| inclination: | 98.3830° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 110.3215° |
| argument of perigee: | 91.0170° |
| revolutions per day: | 14.39062705 |
| mean anomaly at epoch: | 331.4929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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