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 59526U 26145.54898308 +.00000000 +00000-0 +47758-3 0 00007
2 59526 43.0003 243.6681 0002119 281.7072 78.3542 15.27580942 01
| Epoch (UTC): | 25 May 2026 13:10:32 |
| Eccentricity: | 0.0002119 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 243.6681° |
| argument of perigee: | 281.7072° |
| revolutions per day: | 15.27580942 |
| mean anomaly at epoch: | 78.3542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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