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 25544U 26075.87060926 +.00000000 +00000-0 +17131-3 0 00007
2 25544 51.6334 36.8567 0006342 198.5376 161.5382 15.48321468 01
| Epoch (UTC): | 16 March 2026 20:53:40 |
| Eccentricity: | 0.0006342 |
| inclination: | 51.6334° |
| perigee height: | 417 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 36.8567° |
| argument of perigee: | 198.5376° |
| revolutions per day: | 15.48321468 |
| mean anomaly at epoch: | 161.5382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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