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 43803U 26050.11110845 +.00000000 +00000-0 +52433-3 0 00005
2 43803 97.4296 112.7944 0005300 340.7977 19.3062 15.29551883 08
| Epoch (UTC): | 19 February 2026 02:39:59 |
| Eccentricity: | 0.0005300 |
| inclination: | 97.4296° |
| perigee height: | 474 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 112.7944° |
| argument of perigee: | 340.7977° |
| revolutions per day: | 15.29551883 |
| mean anomaly at epoch: | 19.3062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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