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 23337.43449115 .00013612 00000-0 12583-2 0 9997
2 39439 97.7019 298.7645 0054753 75.2154 285.5124 14.93532943541451
| Epoch (UTC): | 03 December 2023 10:25:40 |
| Eccentricity: | 0.0054753 |
| inclination: | 97.7019° |
| perigee height: | 549 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 298.7645° |
| argument of perigee: | 75.2154° |
| revolutions per day: | 14.93532943 |
| mean anomaly at epoch: | 285.5124° |
| orbit number at epoch: | 54145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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