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 39445U 26032.45907652 +.00000000 +00000-0 +61110-3 0 00001
2 39445 97.7807 359.2866 0033327 314.2522 45.5969 15.06057759 04
| Epoch (UTC): | 01 February 2026 11:01:04 |
| Eccentricity: | 0.0033327 |
| inclination: | 97.7807° |
| perigee height: | 525 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 359.2866° |
| argument of perigee: | 314.2522° |
| revolutions per day: | 15.06057759 |
| mean anomaly at epoch: | 45.5969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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