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 58524U 26145.38726382 +.00000000 +00000-0 -84511-5 0 00009
2 58524 43.0040 30.0788 0001353 275.4625 84.6072 15.27581027 01
| Epoch (UTC): | 25 May 2026 09:17:39 |
| Eccentricity: | 0.0001353 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 30.0788° |
| argument of perigee: | 275.4625° |
| revolutions per day: | 15.27581027 |
| mean anomaly at epoch: | 84.6072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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