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 67147U 26145.25544360 +.00000000 +00000-0 +43670-3 0 00008
2 67147 51.9005 102.0439 0000785 74.4260 285.6789 14.79934068 05
| Epoch (UTC): | 25 May 2026 06:07:50 |
| Eccentricity: | 0.0000785 |
| inclination: | 51.9005° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 102.0439° |
| argument of perigee: | 74.4260° |
| revolutions per day: | 14.79934068 |
| mean anomaly at epoch: | 285.6789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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