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 26064.76292891 +.00000000 +00000-0 +10162-3 0 00006
2 32959 98.8648 132.2858 0068298 218.2097 252.4726 14.42986965 06
| Epoch (UTC): | 05 March 2026 18:18:37 |
| Eccentricity: | 0.0068298 |
| inclination: | 98.8648° |
| perigee height: | 700 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 132.2858° |
| argument of perigee: | 218.2097° |
| revolutions per day: | 14.42986965 |
| mean anomaly at epoch: | 252.4726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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