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 58059U 26145.51470606 +.00000000 +00000-0 +53667-4 0 00008
2 58059 43.0059 312.8160 0002341 261.8010 98.2577 15.27569503 00
| Epoch (UTC): | 25 May 2026 12:21:10 |
| Eccentricity: | 0.0002341 |
| inclination: | 43.0059° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 312.8160° |
| argument of perigee: | 261.8010° |
| revolutions per day: | 15.27569503 |
| mean anomaly at epoch: | 98.2577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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