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 26021.42125507 +.00000000 +00000-0 +97957-4 0 00005
2 19275 82.5142 268.9946 0017818 299.6130 60.3311 14.85048171 00
| Epoch (UTC): | 21 January 2026 10:06:36 |
| Eccentricity: | 0.0017818 |
| inclination: | 82.5142° |
| perigee height: | 601 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 268.9946° |
| argument of perigee: | 299.6130° |
| revolutions per day: | 14.85048171 |
| mean anomaly at epoch: | 60.3311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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