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 59192U 26145.66668980 +.00000000 +00000-0 +83180-3 0 00009
2 59192 43.0010 17.8099 0001446 264.4101 108.7670 15.27565621 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001446 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 17.8099° |
| argument of perigee: | 264.4101° |
| revolutions per day: | 15.27565621 |
| mean anomaly at epoch: | 108.7670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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