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 66691U 26145.44453791 +.00000000 +00000-0 +38965-3 0 00000
2 66691 97.4205 219.4856 0006245 85.3732 274.8217 15.20493734 06
| Epoch (UTC): | 25 May 2026 10:40:08 |
| Eccentricity: | 0.0006245 |
| inclination: | 97.4205° |
| perigee height: | 500 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 219.4856° |
| argument of perigee: | 85.3732° |
| revolutions per day: | 15.20493734 |
| mean anomaly at epoch: | 274.8217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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