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 59206U 26145.47327897 +.00000000 +00000-0 +11597-3 0 00006
2 59206 53.1589 158.8090 0001645 112.8765 247.2409 15.30208100 00
| Epoch (UTC): | 25 May 2026 11:21:31 |
| Eccentricity: | 0.0001645 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 158.8090° |
| argument of perigee: | 112.8765° |
| revolutions per day: | 15.30208100 |
| mean anomaly at epoch: | 247.2409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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