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 58197U 26145.20671700 +.00000000 +00000-0 +70766-4 0 00004
2 58197 43.0015 71.5850 0001421 265.1603 94.9087 15.27578575 01
| Epoch (UTC): | 25 May 2026 04:57:40 |
| Eccentricity: | 0.0001421 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.5850° |
| argument of perigee: | 265.1603° |
| revolutions per day: | 15.27578575 |
| mean anomaly at epoch: | 94.9087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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