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 67159U 26145.18252051 +.00000000 +00000-0 +82730-4 0 00007
2 67159 51.9007 107.3784 0000696 71.0739 289.0299 14.79931198 01
| Epoch (UTC): | 25 May 2026 04:22:49 |
| Eccentricity: | 0.0000696 |
| inclination: | 51.9007° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 107.3784° |
| argument of perigee: | 71.0739° |
| revolutions per day: | 14.79931198 |
| mean anomaly at epoch: | 289.0299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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