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 26162.89634601 +.00000000 +00000-0 +31557-4 0 00008
2 27386 98.3833 114.3328 0001339 89.8532 336.4099 14.39063569 05
| Epoch (UTC): | 11 June 2026 21:30:44 |
| Eccentricity: | 0.0001339 |
| inclination: | 98.3833° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 114.3328° |
| argument of perigee: | 89.8532° |
| revolutions per day: | 14.39063569 |
| mean anomaly at epoch: | 336.4099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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