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 65585U 26145.41779627 +.00000000 +00000-0 +17185-3 0 00008
2 65585 81.3060 32.0709 0004522 267.8024 92.2614 13.83269502 05
| Epoch (UTC): | 25 May 2026 10:01:37 |
| Eccentricity: | 0.0004522 |
| inclination: | 81.3060° |
| perigee height: | 949 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 32.0709° |
| argument of perigee: | 267.8024° |
| revolutions per day: | 13.83269502 |
| mean anomaly at epoch: | 92.2614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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