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 26042.21375721 +.00000000 +00000-0 +10225-2 0 00004
2 38745 49.8299 109.1574 1609521 193.2244 162.1104 12.34341807 04
| Epoch (UTC): | 11 February 2026 05:07:48 |
| Eccentricity: | 0.1609521 |
| inclination: | 49.8299° |
| perigee height: | 258 km |
| apogee height: | 2804 km |
| right ascension of ascending node: | 109.1574° |
| argument of perigee: | 193.2244° |
| revolutions per day: | 12.34341807 |
| mean anomaly at epoch: | 162.1104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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