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 44747U 26145.55332434 +.00000000 +00000-0 +38711-3 0 00009
2 44747 53.0418 84.9159 0003548 63.5664 296.5709 15.53391792 08
| Epoch (UTC): | 25 May 2026 13:16:47 |
| Eccentricity: | 0.0003548 |
| inclination: | 53.0418° |
| perigee height: | 404 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 84.9159° |
| argument of perigee: | 63.5664° |
| revolutions per day: | 15.53391792 |
| mean anomaly at epoch: | 296.5709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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