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 43804U 26050.12195722 +.00000000 +00000-0 +45891-3 0 00004
2 43804 97.4356 111.1088 0009817 344.0429 16.0498 15.25432777 07
| Epoch (UTC): | 19 February 2026 02:55:37 |
| Eccentricity: | 0.0009817 |
| inclination: | 97.4356° |
| perigee height: | 483 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 111.1088° |
| argument of perigee: | 344.0429° |
| revolutions per day: | 15.25432777 |
| mean anomaly at epoch: | 16.0498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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