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 36599U 10028B 19083.09986999 .00000010 00000-0 12998-4 0 9997
2 36599 98.3158 301.0719 0056233 135.0275 225.5498 14.56037390464446
| Epoch (UTC): | 24 March 2019 02:23:48 |
| Eccentricity: | 0.0056233 |
| inclination: | 98.3158° |
| perigee height: | 666 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 301.0719° |
| argument of perigee: | 135.0275° |
| revolutions per day: | 14.56037390 |
| mean anomaly at epoch: | 225.5498° |
| orbit number at epoch: | 46444 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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