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 58719U 26145.55929446 +.00000000 +00000-0 +49988-4 0 00007
2 58719 53.1596 232.9335 0000283 27.9126 332.1890 15.30189295 07
| Epoch (UTC): | 25 May 2026 13:25:23 |
| Eccentricity: | 0.0000283 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 232.9335° |
| argument of perigee: | 27.9126° |
| revolutions per day: | 15.30189295 |
| mean anomaly at epoch: | 332.1890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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