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 23338.98100600 .00000488 00000-0 46540-3 0 9996
2 00082 38.8495 192.7051 1163980 71.3512 300.9816 12.26440674963147
| Epoch (UTC): | 04 December 2023 23:32:38 |
| Eccentricity: | 0.1163980 |
| inclination: | 38.8495° |
| perigee height: | 640 km |
| apogee height: | 2489 km |
| right ascension of ascending node: | 192.7051° |
| argument of perigee: | 71.3512° |
| revolutions per day: | 12.26440674 |
| mean anomaly at epoch: | 300.9816° |
| orbit number at epoch: | 96314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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