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 43339U 26140.53169808 +.00000000 +00000-0 +00000-0 0 00008
2 43339 0.0119 319.4010 0000070 299.3161 304.9772 1.00268653 04
| Epoch (UTC): | 20 May 2026 12:45:38 |
| Eccentricity: | 0.0000070 |
| inclination: | 0.0119° |
| perigee height: | 35787 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 319.4010° |
| argument of perigee: | 299.3161° |
| revolutions per day: | 1.00268653 |
| mean anomaly at epoch: | 304.9772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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