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 59547U 26145.38144259 +.00000000 +00000-0 -50347-4 0 00001
2 59547 43.0028 263.4591 0001898 292.4747 67.5904 15.27572542 01
| Epoch (UTC): | 25 May 2026 09:09:16 |
| Eccentricity: | 0.0001898 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.4591° |
| argument of perigee: | 292.4747° |
| revolutions per day: | 15.27572542 |
| mean anomaly at epoch: | 67.5904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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