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 66320U 26145.35311942 +.00000000 +00000-0 +89096-3 0 00001
2 66320 42.9987 139.1703 0001333 266.8271 93.2428 15.27590411 07
| Epoch (UTC): | 25 May 2026 08:28:29 |
| Eccentricity: | 0.0001333 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.1703° |
| argument of perigee: | 266.8271° |
| revolutions per day: | 15.27590411 |
| mean anomaly at epoch: | 93.2428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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