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 66617U 26145.42683341 +.00000000 +00000-0 +39911-3 0 00004
2 66617 53.1571 143.6311 0001143 82.6084 277.5046 15.30205426 05
| Epoch (UTC): | 25 May 2026 10:14:38 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1571° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.6311° |
| argument of perigee: | 82.6084° |
| revolutions per day: | 15.30205426 |
| mean anomaly at epoch: | 277.5046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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