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 19325U 26069.84004053 +.00000000 +00000-0 +85006-4 0 00003
2 19325 82.9549 172.6166 0032367 299.7648 184.2486 13.77909324 02
| Epoch (UTC): | 10 March 2026 20:09:39 |
| Eccentricity: | 0.0032367 |
| inclination: | 82.9549° |
| perigee height: | 948 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 172.6166° |
| argument of perigee: | 299.7648° |
| revolutions per day: | 13.77909324 |
| mean anomaly at epoch: | 184.2486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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