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 39492U 13078C 23338.53971478 .00002891 00000-0 29281-3 0 9994
2 39492 82.4182 83.9422 0019846 128.3047 231.9960 14.90479037537082
| Epoch (UTC): | 04 December 2023 12:57:11 |
| Eccentricity: | 0.0019846 |
| inclination: | 82.4182° |
| perigee height: | 582 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 83.9422° |
| argument of perigee: | 128.3047° |
| revolutions per day: | 14.90479037 |
| mean anomaly at epoch: | 231.9960° |
| orbit number at epoch: | 53708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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