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 26044.93383713 +.00000000 +00000-0 +12234-3 0 00001
2 40376 98.1305 53.7569 0000830 96.5774 263.5523 14.63306912 03
| Epoch (UTC): | 13 February 2026 22:24:43 |
| Eccentricity: | 0.0000830 |
| inclination: | 98.1305° |
| perigee height: | 682 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 53.7569° |
| argument of perigee: | 96.5774° |
| revolutions per day: | 14.63306912 |
| mean anomaly at epoch: | 263.5523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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