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 43803U 26066.39766065 +.00000000 +00000-0 +91182-3 0 00007
2 43803 97.4253 129.0740 0004729 267.8333 92.2366 15.30192720 05
| Epoch (UTC): | 07 March 2026 09:32:37 |
| Eccentricity: | 0.0004729 |
| inclination: | 97.4253° |
| perigee height: | 472 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 129.0740° |
| argument of perigee: | 267.8333° |
| revolutions per day: | 15.30192720 |
| mean anomaly at epoch: | 92.2366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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