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 66934U 26145.33094281 +.00000000 +00000-0 +28403-2 0 00008
2 66934 53.1614 2.2627 0004252 231.5247 128.5373 15.30392003 01
| Epoch (UTC): | 25 May 2026 07:56:33 |
| Eccentricity: | 0.0004252 |
| inclination: | 53.1614° |
| perigee height: | 472 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 2.2627° |
| argument of perigee: | 231.5247° |
| revolutions per day: | 15.30392003 |
| mean anomaly at epoch: | 128.5373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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