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 37789U 26150.52747941 +.00000000 +00000-0 +97476-4 0 00007
2 37789 97.8761 128.2921 0029909 175.8755 328.7378 14.70499274 01
| Epoch (UTC): | 30 May 2026 12:39:34 |
| Eccentricity: | 0.0029909 |
| inclination: | 97.8761° |
| perigee height: | 638 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 128.2921° |
| argument of perigee: | 175.8755° |
| revolutions per day: | 14.70499274 |
| mean anomaly at epoch: | 328.7378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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