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 26017.17633888 +.00000000 +00000-0 +45178-4 0 00006
2 19275 82.5148 272.9840 0018062 314.5454 45.4286 14.85041191 02
| Epoch (UTC): | 17 January 2026 04:13:55 |
| Eccentricity: | 0.0018062 |
| inclination: | 82.5148° |
| perigee height: | 601 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 272.9840° |
| argument of perigee: | 314.5454° |
| revolutions per day: | 14.85041191 |
| mean anomaly at epoch: | 45.4286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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