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 58552U 26145.51237654 +.00000000 +00000-0 +23946-4 0 00007
2 58552 53.1623 65.4535 0001239 83.9263 276.1881 15.34395352 04
| Epoch (UTC): | 25 May 2026 12:17:49 |
| Eccentricity: | 0.0001239 |
| inclination: | 53.1623° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 65.4535° |
| argument of perigee: | 83.9263° |
| revolutions per day: | 15.34395352 |
| mean anomaly at epoch: | 276.1881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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