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 66585U 26145.37493995 +.00000000 +00000-0 +11860-2 0 00008
2 66585 42.9982 274.3442 0001011 270.3574 89.7161 15.27588303 07
| Epoch (UTC): | 25 May 2026 08:59:54 |
| Eccentricity: | 0.0001011 |
| inclination: | 42.9982° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.3442° |
| argument of perigee: | 270.3574° |
| revolutions per day: | 15.27588303 |
| mean anomaly at epoch: | 89.7161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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