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 14760U 84019B 25196.95945312 .00000163 00000-0 63682-4 0 9990
2 14760 74.0431 106.5004 0028161 319.4294 40.4760 14.37022705166965
| Epoch (UTC): | 15 July 2025 23:01:36 |
| Eccentricity: | 0.0028161 |
| inclination: | 74.0431° |
| perigee height: | 748 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 106.5004° |
| argument of perigee: | 319.4294° |
| revolutions per day: | 14.37022705 |
| mean anomaly at epoch: | 40.4760° |
| orbit number at epoch: | 16696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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