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 39417U 26032.44335801 +.00000000 +00000-0 +53385-3 0 00005
2 39417 97.8150 354.0998 0041357 345.0676 14.9322 14.99834211 08
| Epoch (UTC): | 01 February 2026 10:38:26 |
| Eccentricity: | 0.0041357 |
| inclination: | 97.8150° |
| perigee height: | 539 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 354.0998° |
| argument of perigee: | 345.0676° |
| revolutions per day: | 14.99834211 |
| mean anomaly at epoch: | 14.9322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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