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 52632U 26144.82912948 +.00000000 +00000-0 +79843-4 0 00006
2 52632 53.2142 287.3151 0001178 88.5540 271.5588 15.08829240 06
| Epoch (UTC): | 24 May 2026 19:53:56 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 287.3151° |
| argument of perigee: | 88.5540° |
| revolutions per day: | 15.08829240 |
| mean anomaly at epoch: | 271.5588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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