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 66379U 26145.71671801 +.00000000 +00000-0 +23509-3 0 00005
2 66379 52.9937 120.9754 0010837 76.3385 283.8824 15.41220747 05
| Epoch (UTC): | 25 May 2026 17:12:04 |
| Eccentricity: | 0.0010837 |
| inclination: | 52.9937° |
| perigee height: | 435 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 120.9754° |
| argument of perigee: | 76.3385° |
| revolutions per day: | 15.41220747 |
| mean anomaly at epoch: | 283.8824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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