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 39440U 26145.42034475 +.00000000 +00000-0 +33344-3 0 00000
2 39440 97.8896 94.3080 0059572 102.4399 258.3495 14.93554437 00
| Epoch (UTC): | 25 May 2026 10:05:17 |
| Eccentricity: | 0.0059572 |
| inclination: | 97.8896° |
| perigee height: | 545 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 94.3080° |
| argument of perigee: | 102.4399° |
| revolutions per day: | 14.93554437 |
| mean anomaly at epoch: | 258.3495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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