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 14680U 84010B 25193.52126333 -.00000022 00000-0 -38129-4 0 9990
2 14680 82.9560 16.4260 0039158 89.4221 324.3611 13.76696784 81299
| Epoch (UTC): | 12 July 2025 12:30:37 |
| Eccentricity: | 0.0039158 |
| inclination: | 82.9560° |
| perigee height: | 947 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 16.4260° |
| argument of perigee: | 89.4221° |
| revolutions per day: | 13.76696784 |
| mean anomaly at epoch: | 324.3611° |
| orbit number at epoch: | 8129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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