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 40958U 26032.54861698 +.00000000 +00000-0 +17679-3 0 00002
2 40958 97.6624 32.7019 0017166 358.1547 1.9597 14.76562996 04
| Epoch (UTC): | 01 February 2026 13:10:00 |
| Eccentricity: | 0.0017166 |
| inclination: | 97.6624° |
| perigee height: | 628 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 32.7019° |
| argument of perigee: | 358.1547° |
| revolutions per day: | 14.76562996 |
| mean anomaly at epoch: | 1.9597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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