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 56032U 26144.92917687 +.00000000 +00000-0 +17819-4 0 00005
2 56032 43.0044 334.8055 0001597 268.0510 92.0159 15.27576022 08
| Epoch (UTC): | 24 May 2026 22:18:00 |
| Eccentricity: | 0.0001597 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.8055° |
| argument of perigee: | 268.0510° |
| revolutions per day: | 15.27576022 |
| mean anomaly at epoch: | 92.0159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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