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 40376U 26039.60065446 +.00000000 +00000-0 +13438-3 0 00006
2 40376 98.1306 48.4986 0001447 89.8555 270.2813 14.63438443 07
| Epoch (UTC): | 08 February 2026 14:24:56 |
| Eccentricity: | 0.0001447 |
| inclination: | 98.1306° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 48.4986° |
| argument of perigee: | 89.8555° |
| revolutions per day: | 14.63438443 |
| mean anomaly at epoch: | 270.2813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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