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 66766U 26145.44025273 +.00000000 +00000-0 +25000-3 0 00009
2 66766 97.4166 219.5279 0001196 110.0516 250.0848 15.20527926 08
| Epoch (UTC): | 25 May 2026 10:33:57 |
| Eccentricity: | 0.0001196 |
| inclination: | 97.4166° |
| perigee height: | 503 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.5279° |
| argument of perigee: | 110.0516° |
| revolutions per day: | 15.20527926 |
| mean anomaly at epoch: | 250.0848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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