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 32959U 26129.80317491 +.00000000 +00000-0 +41917-4 0 00000
2 32959 98.8553 199.8906 0069264 26.1338 82.9912 14.43019133 00
| Epoch (UTC): | 09 May 2026 19:16:34 |
| Eccentricity: | 0.0069264 |
| inclination: | 98.8553° |
| perigee height: | 699 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 199.8906° |
| argument of perigee: | 26.1338° |
| revolutions per day: | 14.43019133 |
| mean anomaly at epoch: | 82.9912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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