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 67937U 26145.29312986 +.00000000 +00000-0 +77749-3 0 00000
2 67937 42.9987 118.3404 0001245 278.0009 82.0701 15.27582895 02
| Epoch (UTC): | 25 May 2026 07:02:06 |
| Eccentricity: | 0.0001245 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.3404° |
| argument of perigee: | 278.0009° |
| revolutions per day: | 15.27582895 |
| mean anomaly at epoch: | 82.0701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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