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 66378U 26145.71645270 +.00000000 +00000-0 +28923-3 0 00000
2 66378 52.9918 120.9257 0014722 98.7687 261.4984 15.41229187 07
| Epoch (UTC): | 25 May 2026 17:11:41 |
| Eccentricity: | 0.0014722 |
| inclination: | 52.9918° |
| perigee height: | 432 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 120.9257° |
| argument of perigee: | 98.7687° |
| revolutions per day: | 15.41229187 |
| mean anomaly at epoch: | 261.4984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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