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 66631U 26145.38109231 +.00000000 +00000-0 +66795-3 0 00006
2 66631 53.1599 141.9266 0000866 80.2499 279.8602 15.34400335 09
| Epoch (UTC): | 25 May 2026 09:08:46 |
| Eccentricity: | 0.0000866 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 141.9266° |
| argument of perigee: | 80.2499° |
| revolutions per day: | 15.34400335 |
| mean anomaly at epoch: | 279.8602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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