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 39483U 13076A 23275.85121850 .00000013 00000-0 17908-4 0 9996
2 39483 82.4823 64.6057 0019967 89.5495 270.7872 12.42872231443316
| Epoch (UTC): | 02 October 2023 20:25:45 |
| Eccentricity: | 0.0019967 |
| inclination: | 82.4823° |
| perigee height: | 1479 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 64.6057° |
| argument of perigee: | 89.5495° |
| revolutions per day: | 12.42872231 |
| mean anomaly at epoch: | 270.7872° |
| orbit number at epoch: | 44331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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