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 56837U 26145.39317095 +.00000000 +00000-0 -13381-3 0 00007
2 56837 43.0095 33.4681 0001573 269.9663 90.1009 15.27603498 08
| Epoch (UTC): | 25 May 2026 09:26:09 |
| Eccentricity: | 0.0001573 |
| inclination: | 43.0095° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.4681° |
| argument of perigee: | 269.9663° |
| revolutions per day: | 15.27603498 |
| mean anomaly at epoch: | 90.1009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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