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 31126U 07012K 25193.86623880 .00000848 00000-0 17216-3 0 9994
2 31126 98.3808 150.8120 0083716 25.1894 335.3353 14.61699970969249
| Epoch (UTC): | 12 July 2025 20:47:23 |
| Eccentricity: | 0.0083716 |
| inclination: | 98.3808° |
| perigee height: | 628 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 150.8120° |
| argument of perigee: | 25.1894° |
| revolutions per day: | 14.61699970 |
| mean anomaly at epoch: | 335.3353° |
| orbit number at epoch: | 96924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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