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 58489U 26144.85257250 +.00000000 +00000-0 +18588-4 0 00002
2 58489 43.0041 353.5812 0002025 274.7901 85.2720 15.27575243 09
| Epoch (UTC): | 24 May 2026 20:27:42 |
| Eccentricity: | 0.0002025 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 353.5812° |
| argument of perigee: | 274.7901° |
| revolutions per day: | 15.27575243 |
| mean anomaly at epoch: | 85.2720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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