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 26128.19910947 +.00000000 +00000-0 +49355-4 0 00000
2 32959 98.8554 198.2239 0069352 30.8803 30.1125 14.43018642 05
| Epoch (UTC): | 08 May 2026 04:46:43 |
| Eccentricity: | 0.0069352 |
| inclination: | 98.8554° |
| perigee height: | 699 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 198.2239° |
| argument of perigee: | 30.8803° |
| revolutions per day: | 14.43018642 |
| mean anomaly at epoch: | 30.1125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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