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 38745U 26040.43272874 +.00000000 +00000-0 +10750-2 0 00004
2 38745 49.8277 114.8388 1610496 188.4753 168.5492 12.34129891 07
| Epoch (UTC): | 09 February 2026 10:23:07 |
| Eccentricity: | 0.1610496 |
| inclination: | 49.8277° |
| perigee height: | 258 km |
| apogee height: | 2805 km |
| right ascension of ascending node: | 114.8388° |
| argument of perigee: | 188.4753° |
| revolutions per day: | 12.34129891 |
| mean anomaly at epoch: | 168.5492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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