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 data is extracted from the following two-line orbital elements,
1 32959U 08026B 25322.13331544 .00000343 00000-0 11422-3 0 9995
2 32959 98.8841 20.2369 0069037 178.4131 236.1319 14.42916817919647
| Epoch (UTC): | 18 November 2025 03:11:58 |
| Eccentricity: | 0.0069037 |
| inclination: | 98.8841° |
| perigee height: | 699 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 20.2369° |
| argument of perigee: | 178.4131° |
| revolutions per day: | 14.42916817 |
| mean anomaly at epoch: | 236.1319° |
| orbit number at epoch: | 91964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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