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 66395U 26145.42385625 +.00000000 +00000-0 +45428-3 0 00001
2 66395 53.1574 220.4708 0002081 28.6349 331.4766 15.30219375 08
| Epoch (UTC): | 25 May 2026 10:10:21 |
| Eccentricity: | 0.0002081 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 220.4708° |
| argument of perigee: | 28.6349° |
| revolutions per day: | 15.30219375 |
| mean anomaly at epoch: | 331.4766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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