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 40075U 26032.47676206 +.00000000 +00000-0 +22611-3 0 00005
2 40075 98.3873 356.3854 0004686 2.9955 357.1290 14.92816830 03
| Epoch (UTC): | 01 February 2026 11:26:32 |
| Eccentricity: | 0.0004686 |
| inclination: | 98.3873° |
| perigee height: | 586 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 356.3854° |
| argument of perigee: | 2.9955° |
| revolutions per day: | 14.92816830 |
| mean anomaly at epoch: | 357.1290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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