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 46753U 26145.50003470 +.00000000 +00000-0 +52560-3 0 00006
2 46753 53.0391 262.1783 0006898 296.6914 26.3746 15.83467950 01
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0006898 |
| inclination: | 53.0391° |
| perigee height: | 316 km |
| apogee height: | 325 km |
| right ascension of ascending node: | 262.1783° |
| argument of perigee: | 296.6914° |
| revolutions per day: | 15.83467950 |
| mean anomaly at epoch: | 26.3746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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