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 40042U 26108.94952169 +.00000000 +00000-0 +56524-3 0 00000
2 40042 98.0993 129.6934 0007060 11.5454 348.5946 15.31216720 04
| Epoch (UTC): | 18 April 2026 22:47:18 |
| Eccentricity: | 0.0007060 |
| inclination: | 98.0993° |
| perigee height: | 467 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 129.6934° |
| argument of perigee: | 11.5454° |
| revolutions per day: | 15.31216720 |
| mean anomaly at epoch: | 348.5946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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