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 66642U 26145.36996029 +.00000000 +00000-0 +35745-3 0 00006
2 66642 53.1573 143.9786 0001290 72.9901 287.1241 15.30201184 08
| Epoch (UTC): | 25 May 2026 08:52:44 |
| Eccentricity: | 0.0001290 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.9786° |
| argument of perigee: | 72.9901° |
| revolutions per day: | 15.30201184 |
| mean anomaly at epoch: | 287.1241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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