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 58669U 26144.98316314 +.00000000 +00000-0 -44004-5 0 00007
2 58669 43.0023 14.3325 0001188 268.2731 91.7984 15.27556427 05
| Epoch (UTC): | 24 May 2026 23:35:45 |
| Eccentricity: | 0.0001188 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 14.3325° |
| argument of perigee: | 268.2731° |
| revolutions per day: | 15.27556427 |
| mean anomaly at epoch: | 91.7984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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