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 43679U 26140.56573719 +.00000000 +00000-0 +19107-3 0 00009
2 43679 98.0526 352.8377 0000701 233.9777 126.1390 15.16708174 04
| Epoch (UTC): | 20 May 2026 13:34:39 |
| Eccentricity: | 0.0000701 |
| inclination: | 98.0526° |
| perigee height: | 515 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 352.8377° |
| argument of perigee: | 233.9777° |
| revolutions per day: | 15.16708174 |
| mean anomaly at epoch: | 126.1390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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