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 32953U 26075.87044068 +.00000000 +00000-0 +66782-3 0 00004
2 32953 82.5006 52.8538 0019787 149.7192 210.5035 12.43176650 02
| Epoch (UTC): | 16 March 2026 20:53:26 |
| Eccentricity: | 0.0019787 |
| inclination: | 82.5006° |
| perigee height: | 1478 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 52.8538° |
| argument of perigee: | 149.7192° |
| revolutions per day: | 12.43176650 |
| mean anomaly at epoch: | 210.5035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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