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 59664U 26144.91676028 +.00000000 +00000-0 +20767-3 0 00004
2 59664 43.0028 331.0818 0001588 272.5871 87.4799 15.27595703 05
| Epoch (UTC): | 24 May 2026 22:00:08 |
| Eccentricity: | 0.0001588 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.0818° |
| argument of perigee: | 272.5871° |
| revolutions per day: | 15.27595703 |
| mean anomaly at epoch: | 87.4799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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