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 67119U 26145.23427013 +.00000000 +00000-0 +72272-3 0 00000
2 67119 43.0000 96.6262 0001290 275.0778 84.9927 15.27593979 08
| Epoch (UTC): | 25 May 2026 05:37:20 |
| Eccentricity: | 0.0001290 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.6262° |
| argument of perigee: | 275.0778° |
| revolutions per day: | 15.27593979 |
| mean anomaly at epoch: | 84.9927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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