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 26053.86844602 +.00000000 +00000-0 +70516-3 0 00004
2 38734 82.4768 136.4252 0015370 313.5710 46.4093 12.44898049 06
| Epoch (UTC): | 22 February 2026 20:50:33 |
| Eccentricity: | 0.0015370 |
| inclination: | 82.4768° |
| perigee height: | 1474 km |
| apogee height: | 1498 km |
| right ascension of ascending node: | 136.4252° |
| argument of perigee: | 313.5710° |
| revolutions per day: | 12.44898049 |
| mean anomaly at epoch: | 46.4093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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