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 26145.02157667 +.00000000 +00000-0 +26236-3 0 00001
2 66174 51.6363 57.5527 0007748 97.0203 263.1673 15.63802982 00
| Epoch (UTC): | 25 May 2026 00:31:04 |
| Eccentricity: | 0.0007748 |
| inclination: | 51.6363° |
| perigee height: | 371 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 57.5527° |
| argument of perigee: | 97.0203° |
| revolutions per day: | 15.63802982 |
| mean anomaly at epoch: | 263.1673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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