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 43928U 26145.40182774 +.00000000 +00000-0 +80239-4 0 00006
2 43928 86.4492 300.0495 0001593 338.2821 21.8313 14.43597965 08
| Epoch (UTC): | 25 May 2026 09:38:37 |
| Eccentricity: | 0.0001593 |
| inclination: | 86.4492° |
| perigee height: | 746 km |
| apogee height: | 748 km |
| right ascension of ascending node: | 300.0495° |
| argument of perigee: | 338.2821° |
| revolutions per day: | 14.43597965 |
| mean anomaly at epoch: | 21.8313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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