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 66892U 26144.96661691 +.00000000 +00000-0 +70191-3 0 00006
2 66892 53.1597 29.7889 0001192 81.3476 278.7660 15.30192614 06
| Epoch (UTC): | 24 May 2026 23:11:55 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.7889° |
| argument of perigee: | 81.3476° |
| revolutions per day: | 15.30192614 |
| mean anomaly at epoch: | 278.7660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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