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 66344U 26145.35440315 +.00000000 +00000-0 +10586-2 0 00001
2 66344 42.9988 139.1697 0000739 261.9052 98.1716 15.27584741 01
| Epoch (UTC): | 25 May 2026 08:30:20 |
| Eccentricity: | 0.0000739 |
| inclination: | 42.9988° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.1697° |
| argument of perigee: | 261.9052° |
| revolutions per day: | 15.27584741 |
| mean anomaly at epoch: | 98.1716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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