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 55619U 26145.40984193 +.00000000 +00000-0 +87317-6 0 00007
2 55619 43.0017 280.8657 0000987 276.0400 84.0339 15.27573908 06
| Epoch (UTC): | 25 May 2026 09:50:10 |
| Eccentricity: | 0.0000987 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.8657° |
| argument of perigee: | 276.0400° |
| revolutions per day: | 15.27573908 |
| mean anomaly at epoch: | 84.0339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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