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 15453U 84129A 18359.01156010 0.00000000 00000-0 00000-0 0 05
2 15453 15.4964 345.0324 0004725 289.5922 70.3689 0.98851735 04
| Epoch (UTC): | 25 December 2018 00:16:38 |
| Eccentricity: | 0.0004725 |
| inclination: | 15.4964° |
| perigee height: | 36169 km |
| apogee height: | 36209 km |
| right ascension of ascending node: | 345.0324° |
| argument of perigee: | 289.5922° |
| revolutions per day: | 0.98851735 |
| mean anomaly at epoch: | 70.3689° |
| 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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