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 19274U 26037.13062608 +.00000000 +00000-0 +49080-3 0 00004
2 19274 82.4706 295.0125 0011391 290.8412 69.1608 15.31013044 09
| Epoch (UTC): | 06 February 2026 03:08:06 |
| Eccentricity: | 0.0011391 |
| inclination: | 82.4706° |
| perigee height: | 465 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 295.0125° |
| argument of perigee: | 290.8412° |
| revolutions per day: | 15.31013044 |
| mean anomaly at epoch: | 69.1608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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