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 66625U 26145.38319774 +.00000000 +00000-0 +95933-3 0 00000
2 66625 53.1597 141.9421 0001302 83.8390 276.2761 15.34396353 09
| Epoch (UTC): | 25 May 2026 09:11:48 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 141.9421° |
| argument of perigee: | 83.8390° |
| revolutions per day: | 15.34396353 |
| mean anomaly at epoch: | 276.2761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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