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 23947U 96038C 25193.97657880 .00000459 00000-0 29822-3 0 9995
2 23947 55.3088 117.9639 4955352 79.8482 330.5003 5.56800192121670
| Epoch (UTC): | 12 July 2025 23:26:16 |
| Eccentricity: | 0.4955352 |
| inclination: | 55.3088° |
| perigee height: | 405 km |
| apogee height: | 13731 km |
| right ascension of ascending node: | 117.9639° |
| argument of perigee: | 79.8482° |
| revolutions per day: | 5.56800192 |
| mean anomaly at epoch: | 330.5003° |
| orbit number at epoch: | 12167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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