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 34588U 93036WA 24358.00025818 .00002588 00000-0 82027-3 0 9990
2 34588 74.0428 204.8502 0018705 346.9781 129.0333 14.40463063828623
| Epoch (UTC): | 23 December 2024 00:00:22 |
| Eccentricity: | 0.0018705 |
| inclination: | 74.0428° |
| perigee height: | 743 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 204.8502° |
| argument of perigee: | 346.9781° |
| revolutions per day: | 14.40463063 |
| mean anomaly at epoch: | 129.0333° |
| orbit number at epoch: | 82862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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