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 59090U 26145.13024480 +.00000000 +00000-0 +37854-4 0 00007
2 59090 43.0029 192.1917 0001639 262.2771 97.7895 15.27577980 05
| Epoch (UTC): | 25 May 2026 03:07:33 |
| Eccentricity: | 0.0001639 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 192.1917° |
| argument of perigee: | 262.2771° |
| revolutions per day: | 15.27577980 |
| mean anomaly at epoch: | 97.7895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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