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 58952U 26145.19200612 +.00000000 +00000-0 +22968-4 0 00002
2 58952 53.1612 314.1001 0001249 89.6571 270.4574 15.31696805 04
| Epoch (UTC): | 25 May 2026 04:36:29 |
| Eccentricity: | 0.0001249 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 314.1001° |
| argument of perigee: | 89.6571° |
| revolutions per day: | 15.31696805 |
| mean anomaly at epoch: | 270.4574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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