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 59263U 26145.37331588 +.00000000 +00000-0 +24476-4 0 00001
2 59263 53.1597 185.1777 0001258 84.9524 275.1620 15.30193169 02
| Epoch (UTC): | 25 May 2026 08:57:34 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 185.1777° |
| argument of perigee: | 84.9524° |
| revolutions per day: | 15.30193169 |
| mean anomaly at epoch: | 275.1620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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