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 56192U 26145.60420294 +.00000000 +00000-0 +16483-3 0 00006
2 56192 97.3810 35.3933 0011132 287.4259 72.5762 15.25965802 06
| Epoch (UTC): | 25 May 2026 14:30:03 |
| Eccentricity: | 0.0011132 |
| inclination: | 97.3810° |
| perigee height: | 480 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 35.3933° |
| argument of perigee: | 287.4259° |
| revolutions per day: | 15.25965802 |
| mean anomaly at epoch: | 72.5762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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