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 32785U 26145.57560728 +.00000000 +00000-0 +29652-3 0 00003
2 32785 97.8261 126.5298 0010632 103.5655 256.6758 15.09195726 04
| Epoch (UTC): | 25 May 2026 13:48:52 |
| Eccentricity: | 0.0010632 |
| inclination: | 97.8261° |
| perigee height: | 531 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 126.5298° |
| argument of perigee: | 103.5655° |
| revolutions per day: | 15.09195726 |
| mean anomaly at epoch: | 256.6758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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