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 12139U 26140.19097156 +.00000000 +00000-0 +24041-3 0 00004
2 12139 82.9385 223.7660 0251666 289.5245 67.8964 15.13408346 05
| Epoch (UTC): | 20 May 2026 04:34:59 |
| Eccentricity: | 0.0251666 |
| inclination: | 82.9385° |
| perigee height: | 352 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 223.7660° |
| argument of perigee: | 289.5245° |
| revolutions per day: | 15.13408346 |
| mean anomaly at epoch: | 67.8964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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