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 66865U 26145.35092725 +.00000000 +00000-0 +95515-3 0 00003
2 66865 43.0007 270.2041 0001259 271.2006 88.8702 15.27592204 08
| Epoch (UTC): | 25 May 2026 08:25:20 |
| Eccentricity: | 0.0001259 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.2041° |
| argument of perigee: | 271.2006° |
| revolutions per day: | 15.27592204 |
| mean anomaly at epoch: | 88.8702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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