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 52584U 26145.38388317 +.00000000 +00000-0 +24533-4 0 00007
2 52584 53.2152 134.8265 0001404 40.3044 319.8052 15.08845945 04
| Epoch (UTC): | 25 May 2026 09:12:47 |
| Eccentricity: | 0.0001404 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 134.8265° |
| argument of perigee: | 40.3044° |
| revolutions per day: | 15.08845945 |
| mean anomaly at epoch: | 319.8052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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