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 46562U 26145.31485617 +.00000000 +00000-0 +78644-3 0 00001
2 46562 53.0381 103.1925 0008495 53.8782 306.3019 15.68689501 06
| Epoch (UTC): | 25 May 2026 07:33:23 |
| Eccentricity: | 0.0008495 |
| inclination: | 53.0381° |
| perigee height: | 357 km |
| apogee height: | 368 km |
| right ascension of ascending node: | 103.1925° |
| argument of perigee: | 53.8782° |
| revolutions per day: | 15.68689501 |
| mean anomaly at epoch: | 306.3019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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