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 47934U 26145.54694654 +.00000000 +00000-0 +85393-4 0 00003
2 47934 97.5400 29.4844 0016911 41.6508 318.5999 14.98915375 03
| Epoch (UTC): | 25 May 2026 13:07:36 |
| Eccentricity: | 0.0016911 |
| inclination: | 97.5400° |
| perigee height: | 558 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 29.4844° |
| argument of perigee: | 41.6508° |
| revolutions per day: | 14.98915375 |
| mean anomaly at epoch: | 318.5999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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