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 37167U 26150.50715770 +.00000000 +00000-0 +30000-3 0 00009
2 37167 97.9763 131.9299 0018783 351.0241 9.0638 14.90886925 02
| Epoch (UTC): | 30 May 2026 12:10:18 |
| Eccentricity: | 0.0018783 |
| inclination: | 97.9763° |
| perigee height: | 582 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 131.9299° |
| argument of perigee: | 351.0241° |
| revolutions per day: | 14.90886925 |
| mean anomaly at epoch: | 9.0638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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