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 25198.48553170 .00000029 00000-0 12016-4 0 9990
2 13114 82.5398 13.4547 0015519 134.1463 283.3756 13.84773568188715
| Epoch (UTC): | 17 July 2025 11:39:09 |
| Eccentricity: | 0.0015519 |
| inclination: | 82.5398° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 13.4547° |
| argument of perigee: | 134.1463° |
| revolutions per day: | 13.84773568 |
| mean anomaly at epoch: | 283.3756° |
| orbit number at epoch: | 18871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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