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 59954U 26144.68386078 +.00000000 +00000-0 +16580-4 0 00002
2 59954 53.1576 236.4947 0001085 77.7020 282.4120 15.69708254 09
| Epoch (UTC): | 24 May 2026 16:24:45 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1576° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 236.4947° |
| argument of perigee: | 77.7020° |
| revolutions per day: | 15.69708254 |
| mean anomaly at epoch: | 282.4120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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