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 58056U 26144.87882838 +.00000000 +00000-0 +12698-3 0 00005
2 58056 43.0014 316.6417 0001506 263.8406 96.2274 15.27583404 06
| Epoch (UTC): | 24 May 2026 21:05:30 |
| Eccentricity: | 0.0001506 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.6417° |
| argument of perigee: | 263.8406° |
| revolutions per day: | 15.27583404 |
| mean anomaly at epoch: | 96.2274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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