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 65633U 26144.77034130 +.00000000 +00000-0 +89295-3 0 00004
2 65633 53.1599 312.6824 0000901 87.6327 272.4778 15.34405801 04
| Epoch (UTC): | 24 May 2026 18:29:17 |
| Eccentricity: | 0.0000901 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 312.6824° |
| argument of perigee: | 87.6327° |
| revolutions per day: | 15.34405801 |
| mean anomaly at epoch: | 272.4778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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