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 66492U 26145.41544782 +.00000000 +00000-0 +79472-3 0 00005
2 66492 42.9960 277.3498 0001226 129.4397 230.6563 15.27595110 06
| Epoch (UTC): | 25 May 2026 09:58:14 |
| Eccentricity: | 0.0001226 |
| inclination: | 42.9960° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.3498° |
| argument of perigee: | 129.4397° |
| revolutions per day: | 15.27595110 |
| mean anomaly at epoch: | 230.6563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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