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 59203U 26145.66668980 +.00000000 +00000-0 -68694-3 0 00006
2 59203 53.1580 156.5142 0001241 85.9370 255.2595 15.34401659 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.1580° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 156.5142° |
| argument of perigee: | 85.9370° |
| revolutions per day: | 15.34401659 |
| mean anomaly at epoch: | 255.2595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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