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 66497U 26145.66285420 +.00000000 +00000-0 +60802-3 0 00005
2 66497 42.9979 275.7544 0000725 292.9448 67.1327 15.27597999 09
| Epoch (UTC): | 25 May 2026 15:54:30 |
| Eccentricity: | 0.0000725 |
| inclination: | 42.9979° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 275.7544° |
| argument of perigee: | 292.9448° |
| revolutions per day: | 15.27597999 |
| mean anomaly at epoch: | 67.1327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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