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 53632U 26145.51591706 +.00000000 +00000-0 +94321-4 0 00007
2 53632 53.2125 239.2160 0000944 79.0620 281.0478 15.08833385 07
| Epoch (UTC): | 25 May 2026 12:22:55 |
| Eccentricity: | 0.0000944 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 239.2160° |
| argument of perigee: | 79.0620° |
| revolutions per day: | 15.08833385 |
| mean anomaly at epoch: | 281.0478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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