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 59153U 26145.56204146 +.00000000 +00000-0 -27693-4 0 00004
2 59153 43.0039 346.0600 0002069 277.3337 82.7279 15.27583504 07
| Epoch (UTC): | 25 May 2026 13:29:20 |
| Eccentricity: | 0.0002069 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 346.0600° |
| argument of perigee: | 277.3337° |
| revolutions per day: | 15.27583504 |
| mean anomaly at epoch: | 82.7279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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