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 15755U 26137.84205424 +.00000000 +00000-0 +41299-5 0 00004
2 15755 71.1119 340.1257 0034050 28.3974 331.8999 14.21001686 03
| Epoch (UTC): | 17 May 2026 20:12:33 |
| Eccentricity: | 0.0034050 |
| inclination: | 71.1119° |
| perigee height: | 797 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 340.1257° |
| argument of perigee: | 28.3974° |
| revolutions per day: | 14.21001686 |
| mean anomaly at epoch: | 331.8999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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