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 23080.89511410 .00035341 00000-0 12430-2 0 9997
2 37855 101.7054 354.0529 0129383 306.9710 51.9721 15.21616018623263
| Epoch (UTC): | 21 March 2023 21:28:57 |
| Eccentricity: | 0.0129383 |
| inclination: | 101.7054° |
| perigee height: | 412 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 354.0529° |
| argument of perigee: | 306.9710° |
| revolutions per day: | 15.21616018 |
| mean anomaly at epoch: | 51.9721° |
| orbit number at epoch: | 62326 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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