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 58513U 26145.36814007 +.00000000 +00000-0 +90377-5 0 00003
2 58513 43.0035 30.8009 0000935 253.8028 106.2721 15.27577750 09
| Epoch (UTC): | 25 May 2026 08:50:07 |
| Eccentricity: | 0.0000935 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 30.8009° |
| argument of perigee: | 253.8028° |
| revolutions per day: | 15.27577750 |
| mean anomaly at epoch: | 106.2721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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