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 66901U 26145.39754904 +.00000000 +00000-0 +40423-3 0 00000
2 66901 53.1601 27.4946 0001899 103.2808 256.8407 15.34397618 00
| Epoch (UTC): | 25 May 2026 09:32:28 |
| Eccentricity: | 0.0001899 |
| inclination: | 53.1601° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 27.4946° |
| argument of perigee: | 103.2808° |
| revolutions per day: | 15.34397618 |
| mean anomaly at epoch: | 256.8407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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