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 56386U 26145.43324059 +.00000000 +00000-0 +19497-4 0 00003
2 56386 43.0027 124.7377 0001115 262.9067 97.1658 15.27577013 01
| Epoch (UTC): | 25 May 2026 10:23:51 |
| Eccentricity: | 0.0001115 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.7377° |
| argument of perigee: | 262.9067° |
| revolutions per day: | 15.27577013 |
| mean anomaly at epoch: | 97.1658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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