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 43806U 26050.02518427 +.00000000 +00000-0 +30320-3 0 00007
2 43806 97.4164 100.4334 0008005 29.7416 330.4269 15.14474351 03
| Epoch (UTC): | 19 February 2026 00:36:15 |
| Eccentricity: | 0.0008005 |
| inclination: | 97.4164° |
| perigee height: | 517 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 100.4334° |
| argument of perigee: | 29.7416° |
| revolutions per day: | 15.14474351 |
| mean anomaly at epoch: | 330.4269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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