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 39161U 13021C 23343.13874303 .00001388 00000-0 21245-3 0 9998
2 39161 97.8549 50.3640 0010271 123.2075 237.0121 14.75221904568913
| Epoch (UTC): | 09 December 2023 03:19:47 |
| Eccentricity: | 0.0010271 |
| inclination: | 97.8549° |
| perigee height: | 637 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 50.3640° |
| argument of perigee: | 123.2075° |
| revolutions per day: | 14.75221904 |
| mean anomaly at epoch: | 237.0121° |
| orbit number at epoch: | 56891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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