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 55178U 26145.32336957 +.00000000 +00000-0 -25546-2 0 00000
2 55178 87.9163 10.4008 0002223 99.5669 260.5714 13.17643030 01
| Epoch (UTC): | 25 May 2026 07:45:39 |
| Eccentricity: | 0.0002223 |
| inclination: | 87.9163° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4008° |
| argument of perigee: | 99.5669° |
| revolutions per day: | 13.17643030 |
| mean anomaly at epoch: | 260.5714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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