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 18267.50207486 +.00000027 +00000-0 +17001-4 0 9991
2 36599 098.3339 120.8754 0055714 334.7204 025.1260 14.56013629438166
| Epoch (UTC): | 24 September 2018 12:02:59 |
| Eccentricity: | 0.0055714 |
| inclination: | 98.3339° |
| perigee height: | 666 km |
| apogee height: | 745 km |
| right ascension of ascending node: | 120.8754° |
| argument of perigee: | 334.7204° |
| revolutions per day: | 14.56013629 |
| mean anomaly at epoch: | 25.1260° |
| orbit number at epoch: | 43816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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