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 66835U 26145.38405285 +.00000000 +00000-0 +24049-2 0 00005
2 66835 70.0006 141.0955 0003440 272.2935 87.7830 14.98398588 05
| Epoch (UTC): | 25 May 2026 09:13:02 |
| Eccentricity: | 0.0003440 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 141.0955° |
| argument of perigee: | 272.2935° |
| revolutions per day: | 14.98398588 |
| mean anomaly at epoch: | 87.7830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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