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 66886U 26144.95842808 +.00000000 +00000-0 +49967-3 0 00006
2 66886 53.1604 29.7402 0001164 81.0062 279.1072 15.34394874 04
| Epoch (UTC): | 24 May 2026 23:00:08 |
| Eccentricity: | 0.0001164 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 29.7402° |
| argument of perigee: | 81.0062° |
| revolutions per day: | 15.34394874 |
| mean anomaly at epoch: | 279.1072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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