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 58381U 26145.61258811 +.00000000 +00000-0 +58390-3 0 00006
2 58381 53.1619 3.3811 0001210 124.2067 235.9050 15.33340819 05
| Epoch (UTC): | 25 May 2026 14:42:07 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.1619° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 3.3811° |
| argument of perigee: | 124.2067° |
| revolutions per day: | 15.33340819 |
| mean anomaly at epoch: | 235.9050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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