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 66578U 26145.34538767 +.00000000 +00000-0 +74907-3 0 00006
2 66578 43.0009 274.1182 0001188 264.4994 95.5723 15.27594345 07
| Epoch (UTC): | 25 May 2026 08:17:21 |
| Eccentricity: | 0.0001188 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.1182° |
| argument of perigee: | 264.4994° |
| revolutions per day: | 15.27594345 |
| mean anomaly at epoch: | 95.5723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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