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 58378U 26145.53129859 +.00000000 +00000-0 +44368-4 0 00003
2 58378 53.1616 351.5833 0000935 99.3522 260.7585 15.30194138 08
| Epoch (UTC): | 25 May 2026 12:45:04 |
| Eccentricity: | 0.0000935 |
| inclination: | 53.1616° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.5833° |
| argument of perigee: | 99.3522° |
| revolutions per day: | 15.30194138 |
| mean anomaly at epoch: | 260.7585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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