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 65092U 26145.41075366 +.00000000 +00000-0 +65042-3 0 00005
2 65092 53.1590 30.4725 0002034 104.8392 255.2834 15.30203086 01
| Epoch (UTC): | 25 May 2026 09:51:29 |
| Eccentricity: | 0.0002034 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 30.4725° |
| argument of perigee: | 104.8392° |
| revolutions per day: | 15.30203086 |
| mean anomaly at epoch: | 255.2834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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