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 37855U 11061F 23078.85659502 .00033717 00000-0 11904-2 0 9995
2 37855 101.7054 350.8935 0129789 313.1955 45.8480 15.21466586622951
| Epoch (UTC): | 19 March 2023 20:33:29 |
| Eccentricity: | 0.0129789 |
| inclination: | 101.7054° |
| perigee height: | 412 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 350.8935° |
| argument of perigee: | 313.1955° |
| revolutions per day: | 15.21466586 |
| mean anomaly at epoch: | 45.8480° |
| orbit number at epoch: | 62295 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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