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 66257U 26145.65163229 +.00000000 +00000-0 +31778-3 0 00000
2 66257 53.1611 286.1266 0000880 132.5677 227.5399 15.30202000 03
| Epoch (UTC): | 25 May 2026 15:38:21 |
| Eccentricity: | 0.0000880 |
| inclination: | 53.1611° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.1266° |
| argument of perigee: | 132.5677° |
| revolutions per day: | 15.30202000 |
| mean anomaly at epoch: | 227.5399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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