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 47352U 26145.45957370 +.00000000 +00000-0 +12934-3 0 00004
2 47352 53.1598 55.6648 0001347 90.6122 269.5034 15.31698917 02
| Epoch (UTC): | 25 May 2026 11:01:47 |
| Eccentricity: | 0.0001347 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.6648° |
| argument of perigee: | 90.6122° |
| revolutions per day: | 15.31698917 |
| mean anomaly at epoch: | 269.5034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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