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 58046U 26145.46898649 +.00000000 +00000-0 +19364-4 0 00005
2 58046 53.1602 171.1616 0000934 77.0382 283.0725 15.34388053 05
| Epoch (UTC): | 25 May 2026 11:15:20 |
| Eccentricity: | 0.0000934 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 171.1616° |
| argument of perigee: | 77.0382° |
| revolutions per day: | 15.34388053 |
| mean anomaly at epoch: | 283.0725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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