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 66852U 26145.36506222 +.00000000 +00000-0 +61425-3 0 00005
2 66852 42.9963 270.3139 0000846 290.2247 69.8513 15.27611605 07
| Epoch (UTC): | 25 May 2026 08:45:41 |
| Eccentricity: | 0.0000846 |
| inclination: | 42.9963° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.3139° |
| argument of perigee: | 290.2247° |
| revolutions per day: | 15.27611605 |
| mean anomaly at epoch: | 69.8513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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