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 32750U 08014A 23258.01636959 0.00003000 00000-0 11049-3 0 03
2 32750 98.0749 185.1535 0003964 100.2135 259.7863 15.27861749 08
| Epoch (UTC): | 15 September 2023 00:23:34 |
| Eccentricity: | 0.0003964 |
| inclination: | 98.0749° |
| perigee height: | 479 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 185.1535° |
| argument of perigee: | 100.2135° |
| revolutions per day: | 15.27861749 |
| mean anomaly at epoch: | 259.7863° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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