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 26017.90408234 +.00000000 +00000-0 +34039-3 0 00002
2 40043 97.7586 171.6289 0049524 206.5126 153.3555 14.84350758 07
| Epoch (UTC): | 17 January 2026 21:41:52 |
| Eccentricity: | 0.0049524 |
| inclination: | 97.7586° |
| perigee height: | 581 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 171.6289° |
| argument of perigee: | 206.5126° |
| revolutions per day: | 14.84350758 |
| mean anomaly at epoch: | 153.3555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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