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 67375U 26145.22689810 +.00000000 +00000-0 +76870-4 0 00007
2 67375 97.8036 144.2742 0004700 179.9085 180.2134 14.88161586 04
| Epoch (UTC): | 25 May 2026 05:26:43 |
| Eccentricity: | 0.0004700 |
| inclination: | 97.8036° |
| perigee height: | 600 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 144.2742° |
| argument of perigee: | 179.9085° |
| revolutions per day: | 14.88161586 |
| mean anomaly at epoch: | 180.2134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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