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 26144.93121044 +.00000000 +00000-0 +59558-3 0 00001
2 39442 97.5795 138.6638 0015931 34.2137 326.0127 15.32306941 05
| Epoch (UTC): | 24 May 2026 22:20:56 |
| Eccentricity: | 0.0015931 |
| inclination: | 97.5795° |
| perigee height: | 458 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 138.6638° |
| argument of perigee: | 34.2137° |
| revolutions per day: | 15.32306941 |
| mean anomaly at epoch: | 326.0127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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