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 82U 61004B 23337.75915869 .00000650 00000-0 60213-3 0 9995
2 82 38.8497 197.2312 1163975 65.4494 306.2975 12.26439651962996
| Epoch (UTC): | 03 December 2023 18:13:11 |
| Eccentricity: | 0.1163975 |
| inclination: | 38.8497° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 197.2312° |
| argument of perigee: | 65.4494° |
| revolutions per day: | 12.26439651 |
| mean anomaly at epoch: | 306.2975° |
| orbit number at epoch: | 96299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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