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 66365U 26145.41659326 +.00000000 +00000-0 +39575-3 0 00005
2 66365 53.1576 236.0093 0000930 79.8000 280.3106 15.30206504 00
| Epoch (UTC): | 25 May 2026 09:59:53 |
| Eccentricity: | 0.0000930 |
| inclination: | 53.1576° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 236.0093° |
| argument of perigee: | 79.8000° |
| revolutions per day: | 15.30206504 |
| mean anomaly at epoch: | 280.3106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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