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 39442U 26032.45400560 +.00000000 +00000-0 +64649-3 0 00004
2 39442 97.5739 23.9110 0019170 67.6364 292.6904 15.27618456 07
| Epoch (UTC): | 01 February 2026 10:53:46 |
| Eccentricity: | 0.0019170 |
| inclination: | 97.5739° |
| perigee height: | 470 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 23.9110° |
| argument of perigee: | 67.6364° |
| revolutions per day: | 15.27618456 |
| mean anomaly at epoch: | 292.6904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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