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 67168U 26145.56015602 +.00000000 +00000-0 +46600-3 0 00003
2 67168 43.0003 236.4101 0001151 279.5296 80.5426 15.27591074 01
| Epoch (UTC): | 25 May 2026 13:26:37 |
| Eccentricity: | 0.0001151 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.4101° |
| argument of perigee: | 279.5296° |
| revolutions per day: | 15.27591074 |
| mean anomaly at epoch: | 80.5426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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