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 23339.87700980 .00000415 00000-0 40376-3 0 9993
2 00082 38.8494 189.3860 1163986 75.6795 297.0087 12.26441475963250
| Epoch (UTC): | 05 December 2023 21:02:53 |
| Eccentricity: | 0.1163986 |
| inclination: | 38.8494° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 189.3860° |
| argument of perigee: | 75.6795° |
| revolutions per day: | 12.26441475 |
| mean anomaly at epoch: | 297.0087° |
| orbit number at epoch: | 96325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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