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 19275U 26020.74746008 +.00000000 +00000-0 +96701-4 0 00000
2 19275 82.5143 269.6279 0017858 301.9880 57.9600 14.85047167 08
| Epoch (UTC): | 20 January 2026 17:56:20 |
| Eccentricity: | 0.0017858 |
| inclination: | 82.5143° |
| perigee height: | 601 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 269.6279° |
| argument of perigee: | 301.9880° |
| revolutions per day: | 14.85047167 |
| mean anomaly at epoch: | 57.9600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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