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 43927U 26145.57535588 +.00000000 +00000-0 +25238-4 0 00006
2 43927 86.3981 3.0254 0002237 88.9285 271.2167 14.34217295 04
| Epoch (UTC): | 25 May 2026 13:48:30 |
| Eccentricity: | 0.0002237 |
| inclination: | 86.3981° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.0254° |
| argument of perigee: | 88.9285° |
| revolutions per day: | 14.34217295 |
| mean anomaly at epoch: | 271.2167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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