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 26145.40998192 +.00000000 +00000-0 +24705-3 0 00005
2 40043 97.7805 295.9491 0050167 148.0586 212.3688 14.85048952 05
| Epoch (UTC): | 25 May 2026 09:50:22 |
| Eccentricity: | 0.0050167 |
| inclination: | 97.7805° |
| perigee height: | 578 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 295.9491° |
| argument of perigee: | 148.0586° |
| revolutions per day: | 14.85048952 |
| mean anomaly at epoch: | 212.3688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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