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 47311U 21002C 23341.53481206 .00047212 00000-0 70040-3 0 9993
2 47311 60.6744 105.8282 0024486 39.6641 320.6246 15.54560661161071
| Epoch (UTC): | 07 December 2023 12:50:07 |
| Eccentricity: | 0.0024486 |
| inclination: | 60.6744° |
| perigee height: | 387 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 105.8282° |
| argument of perigee: | 39.6641° |
| revolutions per day: | 15.54560661 |
| mean anomaly at epoch: | 320.6246° |
| orbit number at epoch: | 16107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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