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 66233U 26145.62042532 +.00000000 +00000-0 +53971-3 0 00003
2 66233 53.1585 232.8743 0000265 160.8299 199.2712 15.30214254 04
| Epoch (UTC): | 25 May 2026 14:53:24 |
| Eccentricity: | 0.0000265 |
| inclination: | 53.1585° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 232.8743° |
| argument of perigee: | 160.8299° |
| revolutions per day: | 15.30214254 |
| mean anomaly at epoch: | 199.2712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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