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 37192U 26145.46599736 +.00000000 +00000-0 +46374-4 0 00000
2 37192 51.9936 219.3746 0000404 144.7848 229.1596 12.62267024 09
| Epoch (UTC): | 25 May 2026 11:11:02 |
| Eccentricity: | 0.0000404 |
| inclination: | 51.9936° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 219.3746° |
| argument of perigee: | 144.7848° |
| revolutions per day: | 12.62267024 |
| mean anomaly at epoch: | 229.1596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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