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 26144.89400321 +.00000000 +00000-0 +00000-0 0 00006
2 37847 57.0043 342.3932 0003903 11.2637 346.7410 1.70475962 07
| Epoch (UTC): | 24 May 2026 21:27:21 |
| Eccentricity: | 0.0003903 |
| inclination: | 57.0043° |
| perigee height: | 23210 km |
| apogee height: | 23234 km |
| right ascension of ascending node: | 342.3932° |
| argument of perigee: | 11.2637° |
| revolutions per day: | 1.70475962 |
| mean anomaly at epoch: | 346.7410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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