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 37154U 10043C 23088.49480986 .00000045 00000-0 24788-3 0 9998
2 37154 82.4565 78.3370 0014203 358.6215 119.5655 12.43686936569729
| Epoch (UTC): | 29 March 2023 11:52:31 |
| Eccentricity: | 0.0014203 |
| inclination: | 82.4565° |
| perigee height: | 1480 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 78.3370° |
| argument of perigee: | 358.6215° |
| revolutions per day: | 12.43686936 |
| mean anomaly at epoch: | 119.5655° |
| orbit number at epoch: | 56972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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