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 59604U 26145.51772310 +.00000000 +00000-0 +24483-4 0 00006
2 59604 43.0005 320.4677 0001257 274.5396 85.5312 15.27565926 00
| Epoch (UTC): | 25 May 2026 12:25:31 |
| Eccentricity: | 0.0001257 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.4677° |
| argument of perigee: | 274.5396° |
| revolutions per day: | 15.27565926 |
| mean anomaly at epoch: | 85.5312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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