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 66683U 26145.45241244 +.00000000 +00000-0 +13233-3 0 00001
2 66683 97.4249 219.2570 0007520 79.2204 280.9877 15.18248888 04
| Epoch (UTC): | 25 May 2026 10:51:28 |
| Eccentricity: | 0.0007520 |
| inclination: | 97.4249° |
| perigee height: | 506 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 219.2570° |
| argument of perigee: | 79.2204° |
| revolutions per day: | 15.18248888 |
| mean anomaly at epoch: | 280.9877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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