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 59182U 26145.05398617 +.00000000 +00000-0 +14341-3 0 00001
2 59182 43.0038 20.9931 0001644 264.2599 95.8065 15.27584797 09
| Epoch (UTC): | 25 May 2026 01:17:44 |
| Eccentricity: | 0.0001644 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 20.9931° |
| argument of perigee: | 264.2599° |
| revolutions per day: | 15.27584797 |
| mean anomaly at epoch: | 95.8065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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