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 12703U 81053AX 24357.71779235 .00002448 00000-0 13883-2 0 9995
2 12703 82.9692 261.2516 0013834 132.7245 227.5098 14.09597320211015
| Epoch (UTC): | 22 December 2024 17:13:37 |
| Eccentricity: | 0.0013834 |
| inclination: | 82.9692° |
| perigee height: | 851 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 261.2516° |
| argument of perigee: | 132.7245° |
| revolutions per day: | 14.09597320 |
| mean anomaly at epoch: | 227.5098° |
| orbit number at epoch: | 21101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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