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 66575U 26145.35951979 +.00000000 +00000-0 +79293-3 0 00001
2 66575 43.0008 274.2288 0001375 259.7837 100.2860 15.27589980 07
| Epoch (UTC): | 25 May 2026 08:37:42 |
| Eccentricity: | 0.0001375 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.2288° |
| argument of perigee: | 259.7837° |
| revolutions per day: | 15.27589980 |
| mean anomaly at epoch: | 100.2860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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