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 14699U 84013A 25189.19019113 .00004918 00000-0 22581-3 0 9998
2 14699 82.5469 350.0826 0016998 61.2409 299.0530 15.20039334256588
| Epoch (UTC): | 08 July 2025 04:33:52 |
| Eccentricity: | 0.0016998 |
| inclination: | 82.5469° |
| perigee height: | 494 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 350.0826° |
| argument of perigee: | 61.2409° |
| revolutions per day: | 15.20039334 |
| mean anomaly at epoch: | 299.0530° |
| orbit number at epoch: | 25658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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