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 47385U 26145.43216047 +.00000000 +00000-0 +89433-4 0 00006
2 47385 53.1612 40.1583 0001532 97.6126 262.5049 15.31697019 00
| Epoch (UTC): | 25 May 2026 10:22:18 |
| Eccentricity: | 0.0001532 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 40.1583° |
| argument of perigee: | 97.6126° |
| revolutions per day: | 15.31697019 |
| mean anomaly at epoch: | 262.5049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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