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 67141U 26145.28920645 +.00000000 +00000-0 +21660-3 0 00004
2 67141 51.9022 101.9229 0000760 89.2350 270.8700 14.79931164 03
| Epoch (UTC): | 25 May 2026 06:56:27 |
| Eccentricity: | 0.0000760 |
| inclination: | 51.9022° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 101.9229° |
| argument of perigee: | 89.2350° |
| revolutions per day: | 14.79931164 |
| mean anomaly at epoch: | 270.8700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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