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 66517U 26145.55152389 +.00000000 +00000-0 +52317-3 0 00005
2 66517 42.9982 204.2860 0000998 332.0847 27.9951 15.27584732 03
| Epoch (UTC): | 25 May 2026 13:14:11 |
| Eccentricity: | 0.0000998 |
| inclination: | 42.9982° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.2860° |
| argument of perigee: | 332.0847° |
| revolutions per day: | 15.27584732 |
| mean anomaly at epoch: | 27.9951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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