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 66692U 26145.62684043 +.00000000 +00000-0 +24493-3 0 00008
2 66692 97.4213 219.5572 0004733 95.4653 264.7121 15.19437966 01
| Epoch (UTC): | 25 May 2026 15:02:39 |
| Eccentricity: | 0.0004733 |
| inclination: | 97.4213° |
| perigee height: | 504 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 219.5572° |
| argument of perigee: | 95.4653° |
| revolutions per day: | 15.19437966 |
| mean anomaly at epoch: | 264.7121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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