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 13114U 82025B 25194.51174019 .00000019 00000-0 31731-5 0 9996
2 13114 82.5395 16.6183 0015311 144.6441 273.9574 13.84773490188431
| Epoch (UTC): | 13 July 2025 12:16:54 |
| Eccentricity: | 0.0015311 |
| inclination: | 82.5395° |
| perigee height: | 936 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 16.6183° |
| argument of perigee: | 144.6441° |
| revolutions per day: | 13.84773490 |
| mean anomaly at epoch: | 273.9574° |
| orbit number at epoch: | 18843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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