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 26044.93361581 +.00000000 +00000-0 +33160-3 0 00002
2 40043 97.7626 197.9436 0050968 118.5438 242.0921 14.84587751 07
| Epoch (UTC): | 13 February 2026 22:24:24 |
| Eccentricity: | 0.0050968 |
| inclination: | 97.7626° |
| perigee height: | 579 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 197.9436° |
| argument of perigee: | 118.5438° |
| revolutions per day: | 14.84587751 |
| mean anomaly at epoch: | 242.0921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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