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 66655U 26145.35616041 +.00000000 +00000-0 +12501-3 0 00007
2 66655 97.7447 73.9280 0005103 175.0244 185.1025 14.88256248 09
| Epoch (UTC): | 25 May 2026 08:32:52 |
| Eccentricity: | 0.0005103 |
| inclination: | 97.7447° |
| perigee height: | 600 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 73.9280° |
| argument of perigee: | 175.0244° |
| revolutions per day: | 14.88256248 |
| mean anomaly at epoch: | 185.1025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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