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 24255.40736163 .00056981 00000-0 23438-2 0 9998
2 32788 97.5997 236.2634 0004263 166.0084 194.1271 15.23932228891428
| Epoch (UTC): | 11 September 2024 09:46:36 |
| Eccentricity: | 0.0004263 |
| inclination: | 97.5997° |
| perigee height: | 491 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 236.2634° |
| argument of perigee: | 166.0084° |
| revolutions per day: | 15.23932228 |
| mean anomaly at epoch: | 194.1271° |
| orbit number at epoch: | 89142 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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