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 58201U 26145.40839708 +.00000000 +00000-0 +44642-4 0 00000
2 58201 97.8212 153.1088 0002151 97.8429 262.3031 14.87578081 07
| Epoch (UTC): | 25 May 2026 09:48:05 |
| Eccentricity: | 0.0002151 |
| inclination: | 97.8212° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 153.1088° |
| argument of perigee: | 97.8429° |
| revolutions per day: | 14.87578081 |
| mean anomaly at epoch: | 262.3031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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