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 38734U 26160.19399116 +.00000000 +00000-0 +51271-3 0 00001
2 38734 82.4749 69.8174 0017851 78.1498 282.1583 12.44902716 00
| Epoch (UTC): | 09 June 2026 04:39:20 |
| Eccentricity: | 0.0017851 |
| inclination: | 82.4749° |
| perigee height: | 1472 km |
| apogee height: | 1500 km |
| right ascension of ascending node: | 69.8174° |
| argument of perigee: | 78.1498° |
| revolutions per day: | 12.44902716 |
| mean anomaly at epoch: | 282.1583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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