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 58680U 26144.98441816 +.00000000 +00000-0 +22334-3 0 00005
2 58680 42.9998 14.3410 0001313 270.5992 89.4709 15.27592247 06
| Epoch (UTC): | 24 May 2026 23:37:33 |
| Eccentricity: | 0.0001313 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 14.3410° |
| argument of perigee: | 270.5992° |
| revolutions per day: | 15.27592247 |
| mean anomaly at epoch: | 89.4709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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