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 25200.20668095 .00000461 00000-0 44543-4 0 9990
2 11672 82.5153 168.6228 0014810 217.2662 142.7531 14.90536570462810
| Epoch (UTC): | 19 July 2025 04:57:37 |
| Eccentricity: | 0.0014810 |
| inclination: | 82.5153° |
| perigee height: | 586 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 168.6228° |
| argument of perigee: | 217.2662° |
| revolutions per day: | 14.90536570 |
| mean anomaly at epoch: | 142.7531° |
| orbit number at epoch: | 46281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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