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 51964U 26144.97701516 +.00000000 +00000-0 -22918-4 0 00008
2 51964 53.1613 29.4713 0000863 98.6464 261.4635 15.31692497 00
| Epoch (UTC): | 24 May 2026 23:26:54 |
| Eccentricity: | 0.0000863 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 29.4713° |
| argument of perigee: | 98.6464° |
| revolutions per day: | 15.31692497 |
| mean anomaly at epoch: | 261.4635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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