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 66174U 26146.23519728 +.00000000 +00000-0 +29012-3 0 00000
2 66174 51.6375 51.4083 0007157 89.2746 270.9069 15.65005268 01
| Epoch (UTC): | 26 May 2026 05:38:41 |
| Eccentricity: | 0.0007157 |
| inclination: | 51.6375° |
| perigee height: | 368 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 51.4083° |
| argument of perigee: | 89.2746° |
| revolutions per day: | 15.65005268 |
| mean anomaly at epoch: | 270.9069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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