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 26016.36962088 +.00000000 +00000-0 +18173-3 0 00003
2 25544 51.6334 331.0355 0007784 24.7534 335.3826 15.49326051 01
| Epoch (UTC): | 16 January 2026 08:52:15 |
| Eccentricity: | 0.0007784 |
| inclination: | 51.6334° |
| perigee height: | 413 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 331.0355° |
| argument of perigee: | 24.7534° |
| revolutions per day: | 15.49326051 |
| mean anomaly at epoch: | 335.3826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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