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 58349U 26145.63263904 +.00000000 +00000-0 +50314-4 0 00000
2 58349 98.5466 223.8586 0010875 93.0164 267.2266 14.34164624 03
| Epoch (UTC): | 25 May 2026 15:11:00 |
| Eccentricity: | 0.0010875 |
| inclination: | 98.5466° |
| perigee height: | 770 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 223.8586° |
| argument of perigee: | 93.0164° |
| revolutions per day: | 14.34164624 |
| mean anomaly at epoch: | 267.2266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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