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 11672U 80005B 25194.23194690 .00000404 00000-0 38705-4 0 9990
2 11672 82.5146 174.2849 0014439 238.9215 121.0588 14.90531484461927
| Epoch (UTC): | 13 July 2025 05:34:00 |
| Eccentricity: | 0.0014439 |
| inclination: | 82.5146° |
| perigee height: | 586 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 174.2849° |
| argument of perigee: | 238.9215° |
| revolutions per day: | 14.90531484 |
| mean anomaly at epoch: | 121.0588° |
| orbit number at epoch: | 46192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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