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 26076.21734212 +.00000000 +00000-0 +46867-4 0 00001
2 19325 82.9544 167.8777 0032188 281.1776 139.3954 13.77910000 03
| Epoch (UTC): | 17 March 2026 05:12:58 |
| Eccentricity: | 0.0032188 |
| inclination: | 82.9544° |
| perigee height: | 948 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 167.8777° |
| argument of perigee: | 281.1776° |
| revolutions per day: | 13.77910000 |
| mean anomaly at epoch: | 139.3954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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