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 26156.65925344 +.00000000 +00000-0 +47268-4 0 00008
2 27386 98.3829 108.2352 0001350 91.9876 80.9361 14.39061995 01
| Epoch (UTC): | 05 June 2026 15:49:19 |
| Eccentricity: | 0.0001350 |
| inclination: | 98.3829° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 108.2352° |
| argument of perigee: | 91.9876° |
| revolutions per day: | 14.39061995 |
| mean anomaly at epoch: | 80.9361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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