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 66319U 26145.34170240 +.00000000 +00000-0 +57009-3 0 00001
2 66319 42.9998 139.9495 0001463 270.1297 89.9387 15.27589847 00
| Epoch (UTC): | 25 May 2026 08:12:03 |
| Eccentricity: | 0.0001463 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.9495° |
| argument of perigee: | 270.1297° |
| revolutions per day: | 15.27589847 |
| mean anomaly at epoch: | 89.9387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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