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 00082U 61004B 23036.84323369 .00000170 00000-0 19517-3 0 9997
2 00082 38.8500 231.4139 1167208 52.7788 317.3789 12.26090970926057
| Epoch (UTC): | 05 February 2023 20:14:15 |
| Eccentricity: | 0.1167208 |
| inclination: | 38.8500° |
| perigee height: | 639 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 231.4139° |
| argument of perigee: | 52.7788° |
| revolutions per day: | 12.26090970 |
| mean anomaly at epoch: | 317.3789° |
| orbit number at epoch: | 92605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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