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 66847U 26145.40928404 +.00000000 +00000-0 +33164-3 0 00003
2 66847 70.0007 141.1831 0003947 268.0181 92.0526 14.98339946 05
| Epoch (UTC): | 25 May 2026 09:49:22 |
| Eccentricity: | 0.0003947 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.1831° |
| argument of perigee: | 268.0181° |
| revolutions per day: | 14.98339946 |
| mean anomaly at epoch: | 92.0526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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