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 39251U 13048C 23083.75231160 .00000018 00000-0 62806-4 0 9992
2 39251 82.4952 1.5131 0016052 270.0670 89.8567 12.42879044432383
| Epoch (UTC): | 24 March 2023 18:03:19 |
| Eccentricity: | 0.0016052 |
| inclination: | 82.4952° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 1.5131° |
| argument of perigee: | 270.0670° |
| revolutions per day: | 12.42879044 |
| mean anomaly at epoch: | 89.8567° |
| orbit number at epoch: | 43238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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