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 43782U 26050.10187887 +.00000000 +00000-0 +37279-3 0 00001
2 43782 97.4230 105.3682 0010340 357.5774 2.5409 15.19780074 04
| Epoch (UTC): | 19 February 2026 02:26:42 |
| Eccentricity: | 0.0010340 |
| inclination: | 97.4230° |
| perigee height: | 499 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 105.3682° |
| argument of perigee: | 357.5774° |
| revolutions per day: | 15.19780074 |
| mean anomaly at epoch: | 2.5409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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