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 47723U 26145.34239154 +.00000000 +00000-0 -20473-4 0 00006
2 47723 53.1600 130.1860 0001183 121.0824 239.0294 15.31703086 03
| Epoch (UTC): | 25 May 2026 08:13:02 |
| Eccentricity: | 0.0001183 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 130.1860° |
| argument of perigee: | 121.0824° |
| revolutions per day: | 15.31703086 |
| mean anomaly at epoch: | 239.0294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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