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 58604U 26145.19962112 +.00000000 +00000-0 +21385-3 0 00007
2 58604 43.0011 96.6099 0001234 256.6899 103.3815 15.27575294 06
| Epoch (UTC): | 25 May 2026 04:47:27 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.6099° |
| argument of perigee: | 256.6899° |
| revolutions per day: | 15.27575294 |
| mean anomaly at epoch: | 103.3815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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