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 59552U 26145.64715088 +.00000000 +00000-0 +92430-4 0 00008
2 59552 43.0044 268.9328 0001643 287.5479 72.5193 15.27577409 01
| Epoch (UTC): | 25 May 2026 15:31:53 |
| Eccentricity: | 0.0001643 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 268.9328° |
| argument of perigee: | 287.5479° |
| revolutions per day: | 15.27577409 |
| mean anomaly at epoch: | 72.5193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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