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 66580U 26145.40306942 +.00000000 +00000-0 +10057-2 0 00009
2 66580 43.0023 273.6893 0001482 275.9126 84.1557 15.27600465 00
| Epoch (UTC): | 25 May 2026 09:40:25 |
| Eccentricity: | 0.0001482 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.6893° |
| argument of perigee: | 275.9126° |
| revolutions per day: | 15.27600465 |
| mean anomaly at epoch: | 84.1557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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