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 65065U 26145.49651513 +.00000000 +00000-0 +27779-3 0 00002
2 65065 97.4486 222.5006 0001109 231.8446 128.2681 15.05656163 04
| Epoch (UTC): | 25 May 2026 11:54:58 |
| Eccentricity: | 0.0001109 |
| inclination: | 97.4486° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 222.5006° |
| argument of perigee: | 231.8446° |
| revolutions per day: | 15.05656163 |
| mean anomaly at epoch: | 128.2681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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