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 17912U 26129.39568565 +.00000000 +00000-0 +33437-4 0 00004
2 17912 82.5021 239.6070 0018324 327.8942 32.1156 14.85421186 08
| Epoch (UTC): | 09 May 2026 09:29:47 |
| Eccentricity: | 0.0018324 |
| inclination: | 82.5021° |
| perigee height: | 599 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 239.6070° |
| argument of perigee: | 327.8942° |
| revolutions per day: | 14.85421186 |
| mean anomaly at epoch: | 32.1156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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