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 23589U 95027A 18227.60263548 0.00000000 00000-0 00000-0 0 07
2 23589 10.3502 24.7923 0008793 315.2824 44.6910 0.98745085 09
| Epoch (UTC): | 15 August 2018 14:27:47 |
| Eccentricity: | 0.0008793 |
| inclination: | 10.3502° |
| perigee height: | 36182 km |
| apogee height: | 36257 km |
| right ascension of ascending node: | 24.7923° |
| argument of perigee: | 315.2824° |
| revolutions per day: | 0.98745085 |
| mean anomaly at epoch: | 44.6910° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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