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 14096U 83051B 25199.96250737 .00000250 00000-0 44663-3 0 9995
2 14096 72.3010 348.3245 1093302 48.4024 320.5611 12.09944653861112
| Epoch (UTC): | 18 July 2025 23:06:00 |
| Eccentricity: | 0.1093302 |
| inclination: | 72.3010° |
| perigee height: | 760 km |
| apogee height: | 2513 km |
| right ascension of ascending node: | 348.3245° |
| argument of perigee: | 48.4024° |
| revolutions per day: | 12.09944653 |
| mean anomaly at epoch: | 320.5611° |
| orbit number at epoch: | 86111 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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