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 17304U 87006B 24357.72271181 .00000558 00000-0 18928-3 0 9995
2 17304 74.0585 82.2489 0030294 312.2054 47.6529 14.38731862987688
| Epoch (UTC): | 22 December 2024 17:20:42 |
| Eccentricity: | 0.0030294 |
| inclination: | 74.0585° |
| perigee height: | 741 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 82.2489° |
| argument of perigee: | 312.2054° |
| revolutions per day: | 14.38731862 |
| mean anomaly at epoch: | 47.6529° |
| orbit number at epoch: | 98768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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