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 26041.58264777 +.00000000 +00000-0 +77886-3 0 00002
2 66865 43.0052 136.2349 0002360 290.5206 69.5392 15.27601716 00
| Epoch (UTC): | 10 February 2026 13:59:00 |
| Eccentricity: | 0.0002360 |
| inclination: | 43.0052° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 136.2349° |
| argument of perigee: | 290.5206° |
| revolutions per day: | 15.27601716 |
| mean anomaly at epoch: | 69.5392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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