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 66859U 26145.05226272 +.00000000 +00000-0 +57033-3 0 00002
2 66859 43.0014 272.2627 0000878 304.3165 55.7603 15.27592674 05
| Epoch (UTC): | 25 May 2026 01:15:15 |
| Eccentricity: | 0.0000878 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.2627° |
| argument of perigee: | 304.3165° |
| revolutions per day: | 15.27592674 |
| mean anomaly at epoch: | 55.7603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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