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 66975U 26145.46015678 +.00000000 +00000-0 +64957-3 0 00005
2 66975 42.9990 310.3100 0000847 248.0750 112.0012 15.27601189 08
| Epoch (UTC): | 25 May 2026 11:02:37 |
| Eccentricity: | 0.0000847 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 310.3100° |
| argument of perigee: | 248.0750° |
| revolutions per day: | 15.27601189 |
| mean anomaly at epoch: | 112.0012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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