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 26151.83448264 +.00000000 +00000-0 +51143-4 0 00001
2 27386 98.3829 103.5184 0001303 92.4711 299.6173 14.39060590 04
| Epoch (UTC): | 31 May 2026 20:01:39 |
| Eccentricity: | 0.0001303 |
| inclination: | 98.3829° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 103.5184° |
| argument of perigee: | 92.4711° |
| revolutions per day: | 14.39060590 |
| mean anomaly at epoch: | 299.6173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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