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 53589U 26145.06143128 +.00000000 +00000-0 +47859-4 0 00003
2 53589 53.2159 261.3240 0001250 89.7886 270.3249 15.08840787 04
| Epoch (UTC): | 25 May 2026 01:28:27 |
| Eccentricity: | 0.0001250 |
| inclination: | 53.2159° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 261.3240° |
| argument of perigee: | 89.7886° |
| revolutions per day: | 15.08840787 |
| mean anomaly at epoch: | 270.3249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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