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 59546U 26145.35605579 +.00000000 +00000-0 +95631-4 0 00008
2 59546 43.0003 270.1950 0001195 268.2494 91.8221 15.27582935 06
| Epoch (UTC): | 25 May 2026 08:32:43 |
| Eccentricity: | 0.0001195 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.1950° |
| argument of perigee: | 268.2494° |
| revolutions per day: | 15.27582935 |
| mean anomaly at epoch: | 91.8221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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