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 26106.66489604 +.00000000 +00000-0 +14511-3 0 00007
2 40043 97.7747 258.1245 0048096 276.5548 83.0193 14.84902111 00
| Epoch (UTC): | 16 April 2026 15:57:27 |
| Eccentricity: | 0.0048096 |
| inclination: | 97.7747° |
| perigee height: | 580 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 258.1245° |
| argument of perigee: | 276.5548° |
| revolutions per day: | 14.84902111 |
| mean anomaly at epoch: | 83.0193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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