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 37847U 26142.53932333 +.00000000 +00000-0 +00000-0 0 00008
2 37847 57.0051 342.4570 0003957 10.6437 342.2407 1.70475888 09
| Epoch (UTC): | 22 May 2026 12:56:37 |
| Eccentricity: | 0.0003957 |
| inclination: | 57.0051° |
| perigee height: | 23210 km |
| apogee height: | 23234 km |
| right ascension of ascending node: | 342.4570° |
| argument of perigee: | 10.6437° |
| revolutions per day: | 1.70475888 |
| mean anomaly at epoch: | 342.2407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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