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 67061U 26145.29370076 +.00000000 +00000-0 +91520-4 0 00006
2 67061 49.9990 107.7660 0000840 353.7844 6.3018 13.29327142 07
| Epoch (UTC): | 25 May 2026 07:02:55 |
| Eccentricity: | 0.0000840 |
| inclination: | 49.9990° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 107.7660° |
| argument of perigee: | 353.7844° |
| revolutions per day: | 13.29327142 |
| mean anomaly at epoch: | 6.3018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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