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 58199U 26145.40839597 +.00000000 +00000-0 +44799-4 0 00005
2 58199 97.8213 153.1048 0001564 90.0917 270.0479 14.87578092 08
| Epoch (UTC): | 25 May 2026 09:48:05 |
| Eccentricity: | 0.0001564 |
| inclination: | 97.8213° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 153.1048° |
| argument of perigee: | 90.0917° |
| revolutions per day: | 14.87578092 |
| mean anomaly at epoch: | 270.0479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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