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 59171U 26144.93814860 +.00000000 +00000-0 +98665-4 0 00000
2 59171 43.0075 36.6849 0001479 255.2689 104.7999 15.27569352 02
| Epoch (UTC): | 24 May 2026 22:30:56 |
| Eccentricity: | 0.0001479 |
| inclination: | 43.0075° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 36.6849° |
| argument of perigee: | 255.2689° |
| revolutions per day: | 15.27569352 |
| mean anomaly at epoch: | 104.7999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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