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 66610U 26145.24318779 +.00000000 +00000-0 +68448-3 0 00004
2 66610 43.0006 343.8527 0002290 278.0817 81.9775 15.27602200 04
| Epoch (UTC): | 25 May 2026 05:50:11 |
| Eccentricity: | 0.0002290 |
| inclination: | 43.0006° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 343.8527° |
| argument of perigee: | 278.0817° |
| revolutions per day: | 15.27602200 |
| mean anomaly at epoch: | 81.9775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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