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 14373U 83099B 25198.51592466 .00000390 00000-0 41823-4 0 9994
2 14373 82.5394 3.1893 0019024 192.5722 167.5023 14.85911155237690
| Epoch (UTC): | 17 July 2025 12:22:55 |
| Eccentricity: | 0.0019024 |
| inclination: | 82.5394° |
| perigee height: | 597 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 3.1893° |
| argument of perigee: | 192.5722° |
| revolutions per day: | 14.85911155 |
| mean anomaly at epoch: | 167.5023° |
| orbit number at epoch: | 23769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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