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 23338.89955037 .00000495 00000-0 47078-3 0 9993
2 00082 38.8496 193.0069 1163981 70.9580 301.3393 12.26440586963138
| Epoch (UTC): | 04 December 2023 21:35:21 |
| Eccentricity: | 0.1163981 |
| inclination: | 38.8496° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 193.0069° |
| argument of perigee: | 70.9580° |
| revolutions per day: | 12.26440586 |
| mean anomaly at epoch: | 301.3393° |
| orbit number at epoch: | 96313 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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