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 43929U 26145.34702389 +.00000000 +00000-0 +23665-4 0 00000
2 43929 86.3993 3.4246 0002118 83.4267 276.7170 14.34218202 05
| Epoch (UTC): | 25 May 2026 08:19:42 |
| Eccentricity: | 0.0002118 |
| inclination: | 86.3993° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.4246° |
| argument of perigee: | 83.4267° |
| revolutions per day: | 14.34218202 |
| mean anomaly at epoch: | 276.7170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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