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 32788U 08021F 24252.51791941 .00059968 00000-0 24920-2 0 9997
2 32788 97.5999 233.3361 0003482 175.5294 184.5974 15.23573773891086
| Epoch (UTC): | 08 September 2024 12:25:48 |
| Eccentricity: | 0.0003482 |
| inclination: | 97.5999° |
| perigee height: | 492 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 233.3361° |
| argument of perigee: | 175.5294° |
| revolutions per day: | 15.23573773 |
| mean anomaly at epoch: | 184.5974° |
| orbit number at epoch: | 89108 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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