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 32951U 26145.33517000 +.00000000 +00000-0 +00000-0 0 00000
2 32951 0.0333 110.8540 0003048 319.2028 170.5133 1.00270243 09
| Epoch (UTC): | 25 May 2026 08:02:38 |
| Eccentricity: | 0.0003048 |
| inclination: | 0.0333° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 110.8540° |
| argument of perigee: | 319.2028° |
| revolutions per day: | 1.00270243 |
| mean anomaly at epoch: | 170.5133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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