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 66447U 26145.43529884 +.00000000 +00000-0 +40037-3 0 00008
2 66447 42.9979 201.3423 0000705 272.7716 87.3054 15.27592350 04
| Epoch (UTC): | 25 May 2026 10:26:49 |
| Eccentricity: | 0.0000705 |
| inclination: | 42.9979° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 201.3423° |
| argument of perigee: | 272.7716° |
| revolutions per day: | 15.27592350 |
| mean anomaly at epoch: | 87.3054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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