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 31974U 99025CPB 24357.51484979 .00010376 00000-0 43540-2 0 9992
2 31974 98.3990 17.0083 0077018 269.1543 90.0812 14.24480532643552
| Epoch (UTC): | 22 December 2024 12:21:23 |
| Eccentricity: | 0.0077018 |
| inclination: | 98.3990° |
| perigee height: | 755 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 17.0083° |
| argument of perigee: | 269.1543° |
| revolutions per day: | 14.24480532 |
| mean anomaly at epoch: | 90.0812° |
| orbit number at epoch: | 64355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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