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 40766U 26019.70997317 +.00000000 +00000-0 +43993-3 0 00008
2 40766 102.1491 284.9390 0101432 112.9055 273.1935 12.23242537 03
| Epoch (UTC): | 19 January 2026 17:02:21 |
| Eccentricity: | 0.0101432 |
| inclination: | 102.1491° |
| perigee height: | 1498 km |
| apogee height: | 1659 km |
| right ascension of ascending node: | 284.9390° |
| argument of perigee: | 112.9055° |
| revolutions per day: | 12.23242537 |
| mean anomaly at epoch: | 273.1935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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