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 32289U 07055A 23267.11088529 .00002986 00000-0 37067-3 0 9996
2 32289 97.9159 289.9593 0001987 92.2141 267.9300 14.83364659857719
| Epoch (UTC): | 24 September 2023 02:39:40 |
| Eccentricity: | 0.0001987 |
| inclination: | 97.9159° |
| perigee height: | 617 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 289.9593° |
| argument of perigee: | 92.2141° |
| revolutions per day: | 14.83364659 |
| mean anomaly at epoch: | 267.9300° |
| orbit number at epoch: | 85771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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