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 66729U 26145.45716356 +.00000000 +00000-0 +26962-3 0 00006
2 66729 97.4197 219.2742 0006556 92.3980 267.8005 15.19288863 08
| Epoch (UTC): | 25 May 2026 10:58:18 |
| Eccentricity: | 0.0006556 |
| inclination: | 97.4197° |
| perigee height: | 503 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 219.2742° |
| argument of perigee: | 92.3980° |
| revolutions per day: | 15.19288863 |
| mean anomaly at epoch: | 267.8005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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