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 39439U 13066Z 23334.82153481 .00017878 00000-0 16539-2 0 9998
2 39439 97.7014 296.2037 0054927 83.3959 277.3510 14.93432963542157
| Epoch (UTC): | 30 November 2023 19:43:00 |
| Eccentricity: | 0.0054927 |
| inclination: | 97.7014° |
| perigee height: | 549 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 296.2037° |
| argument of perigee: | 83.3959° |
| revolutions per day: | 14.93432963 |
| mean anomaly at epoch: | 277.3510° |
| orbit number at epoch: | 54215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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