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 26039.80577336 +.00000000 +00000-0 +13567-3 0 00007
2 40376 98.1306 48.7008 0001446 89.7390 270.3978 14.63438736 08
| Epoch (UTC): | 08 February 2026 19:20:18 |
| Eccentricity: | 0.0001446 |
| inclination: | 98.1306° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 48.7008° |
| argument of perigee: | 89.7390° |
| revolutions per day: | 14.63438736 |
| mean anomaly at epoch: | 270.3978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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