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 18265.95087639 0.00000000 00000-0 00000-0 0 04
2 15453 15.5636 346.0156 0004090 283.7491 76.1952 0.98849944 03
| Epoch (UTC): | 22 September 2018 22:49:15 |
| Eccentricity: | 0.0004090 |
| inclination: | 15.5636° |
| perigee height: | 36172 km |
| apogee height: | 36207 km |
| right ascension of ascending node: | 346.0156° |
| argument of perigee: | 283.7491° |
| revolutions per day: | 0.98849944 |
| mean anomaly at epoch: | 76.1952° |
| 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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