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 26144.86403750 +.00000000 +00000-0 +44853-3 0 00005
2 39445 97.7948 113.0441 0031552 291.4400 68.3463 15.07948407 06
| Epoch (UTC): | 24 May 2026 20:44:12 |
| Eccentricity: | 0.0031552 |
| inclination: | 97.7948° |
| perigee height: | 521 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 113.0441° |
| argument of perigee: | 291.4400° |
| revolutions per day: | 15.07948407 |
| mean anomaly at epoch: | 68.3463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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