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 24357.90601086 .00000806 00000-0 47401-3 0 9992
2 00012 32.9007 331.2899 1651082 120.9476 256.3808 11.47488205469105
| Epoch (UTC): | 22 December 2024 21:44:39 |
| Eccentricity: | 0.1651082 |
| inclination: | 32.9007° |
| perigee height: | 554 km |
| apogee height: | 3296 km |
| right ascension of ascending node: | 331.2899° |
| argument of perigee: | 120.9476° |
| revolutions per day: | 11.47488205 |
| mean anomaly at epoch: | 256.3808° |
| orbit number at epoch: | 46910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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