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 58385U 26145.34013161 +.00000000 +00000-0 -76195-5 0 00003
2 58385 53.1600 3.8593 0001385 74.5144 285.6012 15.34380925 00
| Epoch (UTC): | 25 May 2026 08:09:47 |
| Eccentricity: | 0.0001385 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 3.8593° |
| argument of perigee: | 74.5144° |
| revolutions per day: | 15.34380925 |
| mean anomaly at epoch: | 285.6012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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