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 58517U 26145.37313400 +.00000000 +00000-0 -11510-4 0 00001
2 58517 43.0028 29.9753 0001079 275.7670 84.3059 15.27579399 07
| Epoch (UTC): | 25 May 2026 08:57:18 |
| Eccentricity: | 0.0001079 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 29.9753° |
| argument of perigee: | 275.7670° |
| revolutions per day: | 15.27579399 |
| mean anomaly at epoch: | 84.3059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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