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 66347U 26145.29416576 +.00000000 +00000-0 +53582-3 0 00003
2 66347 42.9989 139.5747 0000961 280.6438 79.4305 15.27607877 00
| Epoch (UTC): | 25 May 2026 07:03:35 |
| Eccentricity: | 0.0000961 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.5747° |
| argument of perigee: | 280.6438° |
| revolutions per day: | 15.27607877 |
| mean anomaly at epoch: | 79.4305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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