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 67658U 26145.04922723 +.00000000 +00000-0 +46088-3 0 00001
2 67658 97.2846 178.2855 0001194 141.8286 218.3042 15.33434397 03
| Epoch (UTC): | 25 May 2026 01:10:53 |
| Eccentricity: | 0.0001194 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.2855° |
| argument of perigee: | 141.8286° |
| revolutions per day: | 15.33434397 |
| mean anomaly at epoch: | 218.3042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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