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 47734U 26145.45468063 +.00000000 +00000-0 +16579-3 0 00003
2 47734 53.1581 206.8636 0001196 84.2330 275.8808 15.31709111 05
| Epoch (UTC): | 25 May 2026 10:54:44 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 206.8636° |
| argument of perigee: | 84.2330° |
| revolutions per day: | 15.31709111 |
| mean anomaly at epoch: | 275.8808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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