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 23340.61009229 .00000351 00000-0 34933-3 0 9996
2 00082 38.8493 186.6704 1163990 79.2204 293.7093 12.26441989963346
| Epoch (UTC): | 06 December 2023 14:38:31 |
| Eccentricity: | 0.1163990 |
| inclination: | 38.8493° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 186.6704° |
| argument of perigee: | 79.2204° |
| revolutions per day: | 12.26441989 |
| mean anomaly at epoch: | 293.7093° |
| orbit number at epoch: | 96334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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