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 40043U 26156.39259148 +.00000000 +00000-0 +29106-3 0 00006
2 40043 97.7823 306.6759 0050661 112.8276 247.8301 14.85113629 05
| Epoch (UTC): | 05 June 2026 09:25:19 |
| Eccentricity: | 0.0050661 |
| inclination: | 97.7823° |
| perigee height: | 578 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 306.6759° |
| argument of perigee: | 112.8276° |
| revolutions per day: | 14.85113629 |
| mean anomaly at epoch: | 247.8301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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