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 65892U 26145.34235476 +.00000000 +00000-0 -18516-4 0 00001
2 65892 53.1592 14.3561 0001468 101.4081 258.7087 15.34382803 05
| Epoch (UTC): | 25 May 2026 08:12:59 |
| Eccentricity: | 0.0001468 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 14.3561° |
| argument of perigee: | 101.4081° |
| revolutions per day: | 15.34382803 |
| mean anomaly at epoch: | 258.7087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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