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 is defined by the following mean orbital elements,
1 13114U 26159.36284990 +.00000000 +00000-0 +27490-4 0 00003
2 13114 82.5392 114.1118 0013477 305.6823 165.2896 13.84790597 07
| Epoch (UTC): | 08 June 2026 08:42:30 |
| Eccentricity: | 0.0013477 |
| inclination: | 82.5392° |
| perigee height: | 937 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 114.1118° |
| argument of perigee: | 305.6823° |
| revolutions per day: | 13.84790597 |
| mean anomaly at epoch: | 165.2896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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