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 67668U 26145.37004855 +.00000000 +00000-0 +36725-3 0 00002
2 67668 97.2851 178.6160 0000688 102.0094 258.1226 15.33450388 00
| Epoch (UTC): | 25 May 2026 08:52:52 |
| Eccentricity: | 0.0000688 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6160° |
| argument of perigee: | 102.0094° |
| revolutions per day: | 15.33450388 |
| mean anomaly at epoch: | 258.1226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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