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 14760U 26127.87972476 +.00000000 +00000-0 +58108-4 0 00005
2 14760 74.0419 282.4816 0026681 63.7092 296.6798 14.37198935 03
| Epoch (UTC): | 07 May 2026 21:06:48 |
| Eccentricity: | 0.0026681 |
| inclination: | 74.0419° |
| perigee height: | 749 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 282.4816° |
| argument of perigee: | 63.7092° |
| revolutions per day: | 14.37198935 |
| mean anomaly at epoch: | 296.6798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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