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 67139U 26145.22453941 +.00000000 +00000-0 +33803-3 0 00007
2 67139 51.8989 81.9660 0001833 120.0073 240.1070 14.76457049 07
| Epoch (UTC): | 25 May 2026 05:23:20 |
| Eccentricity: | 0.0001833 |
| inclination: | 51.8989° |
| perigee height: | 639 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 81.9660° |
| argument of perigee: | 120.0073° |
| revolutions per day: | 14.76457049 |
| mean anomaly at epoch: | 240.1070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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