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 21023.88944262 -.00000009 00000-0 87877-5 0 9996
2 36599 98.2304 247.2844 0054548 217.7572 141.9793 14.56120379562205
| Epoch (UTC): | 23 January 2021 21:20:47 |
| Eccentricity: | 0.0054548 |
| inclination: | 98.2304° |
| perigee height: | 667 km |
| apogee height: | 744 km |
| right ascension of ascending node: | 247.2844° |
| argument of perigee: | 217.7572° |
| revolutions per day: | 14.56120379 |
| mean anomaly at epoch: | 141.9793° |
| orbit number at epoch: | 56220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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