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 23336.86312083 .00000645 00000-0 59834-3 0 9996
2 00082 38.8499 200.5503 1163971 61.1209 310.1264 12.26438013962885
| Epoch (UTC): | 02 December 2023 20:42:53 |
| Eccentricity: | 0.1163971 |
| inclination: | 38.8499° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 200.5503° |
| argument of perigee: | 61.1209° |
| revolutions per day: | 12.26438013 |
| mean anomaly at epoch: | 310.1264° |
| orbit number at epoch: | 96288 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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