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 66325U 26145.47632755 +.00000000 +00000-0 +62073-3 0 00003
2 66325 43.0003 139.2353 0001470 272.9016 87.1667 15.27593419 00
| Epoch (UTC): | 25 May 2026 11:25:54 |
| Eccentricity: | 0.0001470 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.2353° |
| argument of perigee: | 272.9016° |
| revolutions per day: | 15.27593419 |
| mean anomaly at epoch: | 87.1667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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