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 66608U 26144.96365582 +.00000000 +00000-0 +61153-3 0 00009
2 66608 43.0014 345.1897 0001755 272.6455 87.4195 15.27598568 06
| Epoch (UTC): | 24 May 2026 23:07:39 |
| Eccentricity: | 0.0001755 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.1897° |
| argument of perigee: | 272.6455° |
| revolutions per day: | 15.27598568 |
| mean anomaly at epoch: | 87.4195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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