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 32791U 08021J 24259.41660682 .00022443 00000-0 15030-2 0 9994
2 32791 97.6977 230.2844 0005696 35.1550 325.0052 15.06899014890093
| Epoch (UTC): | 15 September 2024 09:59:54 |
| Eccentricity: | 0.0005696 |
| inclination: | 97.6977° |
| perigee height: | 542 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 230.2844° |
| argument of perigee: | 35.1550° |
| revolutions per day: | 15.06899014 |
| mean anomaly at epoch: | 325.0052° |
| orbit number at epoch: | 89009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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