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 47393U 26145.66668980 +.00000000 +00000-0 +99365-3 0 00001
2 47393 53.0324 319.4251 0006378 261.3510 122.3203 15.91701806 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0006378 |
| inclination: | 53.0324° |
| perigee height: | 293 km |
| apogee height: | 302 km |
| right ascension of ascending node: | 319.4251° |
| argument of perigee: | 261.3510° |
| revolutions per day: | 15.91701806 |
| mean anomaly at epoch: | 122.3203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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