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 27665U 26017.24538389 +.00000000 +00000-0 +51233-4 0 00005
2 27665 39.5772 334.7872 0008455 147.7909 346.5131 14.29500657 06
| Epoch (UTC): | 17 January 2026 05:53:21 |
| Eccentricity: | 0.0008455 |
| inclination: | 39.5772° |
| perigee height: | 787 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 334.7872° |
| argument of perigee: | 147.7909° |
| revolutions per day: | 14.29500657 |
| mean anomaly at epoch: | 346.5131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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