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 47789U 26145.31430855 +.00000000 +00000-0 +29554-4 0 00004
2 47789 53.1593 242.9259 0001699 84.5921 275.5274 15.31699581 00
| Epoch (UTC): | 25 May 2026 07:32:36 |
| Eccentricity: | 0.0001699 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 242.9259° |
| argument of perigee: | 84.5921° |
| revolutions per day: | 15.31699581 |
| mean anomaly at epoch: | 275.5274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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