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 00012U 59001B 23340.15804470 .00000530 00000-0 28759-3 0 9991
2 00012 32.9101 235.6162 1660399 260.8142 80.1694 11.45890575425164
| Epoch (UTC): | 06 December 2023 03:47:35 |
| Eccentricity: | 0.1660399 |
| inclination: | 32.9101° |
| perigee height: | 552 km |
| apogee height: | 3312 km |
| right ascension of ascending node: | 235.6162° |
| argument of perigee: | 260.8142° |
| revolutions per day: | 11.45890575 |
| mean anomaly at epoch: | 80.1694° |
| orbit number at epoch: | 42516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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