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 66323U 26145.47377052 +.00000000 +00000-0 +55135-3 0 00008
2 66323 43.0002 139.2102 0001365 262.7916 97.2781 15.27574805 05
| Epoch (UTC): | 25 May 2026 11:22:13 |
| Eccentricity: | 0.0001365 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.2102° |
| argument of perigee: | 262.7916° |
| revolutions per day: | 15.27574805 |
| mean anomaly at epoch: | 97.2781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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