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 37788U 11044A 23338.18665392 .00001776 00000-0 28338-3 0 9990
2 37788 98.3861 193.7247 0036632 185.4221 288.9090 14.72821179660039
| Epoch (UTC): | 04 December 2023 04:28:46 |
| Eccentricity: | 0.0036632 |
| inclination: | 98.3861° |
| perigee height: | 626 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 193.7247° |
| argument of perigee: | 185.4221° |
| revolutions per day: | 14.72821179 |
| mean anomaly at epoch: | 288.9090° |
| orbit number at epoch: | 66003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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