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 23272.02125895 .00037467 00000-0 99332-3 0 9991
2 37855 101.7087 292.8394 0106116 80.8776 280.4439 15.32638939652903
| Epoch (UTC): | 29 September 2023 00:30:36 |
| Eccentricity: | 0.0106116 |
| inclination: | 101.7087° |
| perigee height: | 395 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 292.8394° |
| argument of perigee: | 80.8776° |
| revolutions per day: | 15.32638939 |
| mean anomaly at epoch: | 280.4439° |
| orbit number at epoch: | 65290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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