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 59123U 26145.33367916 +.00000000 +00000-0 +16549-3 0 00007
2 59123 97.5563 281.9026 0009197 333.4296 26.6472 15.30901694 06
| Epoch (UTC): | 25 May 2026 08:00:29 |
| Eccentricity: | 0.0009197 |
| inclination: | 97.5563° |
| perigee height: | 467 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 281.9026° |
| argument of perigee: | 333.4296° |
| revolutions per day: | 15.30901694 |
| mean anomaly at epoch: | 26.6472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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