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 25198.53789541 -.00000014 00000-0 -30534-4 0 9995
2 14680 82.9562 12.7055 0039098 75.8955 346.8175 13.76696514 81989
| Epoch (UTC): | 17 July 2025 12:54:34 |
| Eccentricity: | 0.0039098 |
| inclination: | 82.9562° |
| perigee height: | 947 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 12.7055° |
| argument of perigee: | 75.8955° |
| revolutions per day: | 13.76696514 |
| mean anomaly at epoch: | 346.8175° |
| orbit number at epoch: | 8198 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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