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 67126U 26145.23171736 +.00000000 +00000-0 +10500-3 0 00002
2 67126 43.0016 96.6006 0002257 258.1478 101.9121 15.27544144 08
| Epoch (UTC): | 25 May 2026 05:33:40 |
| Eccentricity: | 0.0002257 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 96.6006° |
| argument of perigee: | 258.1478° |
| revolutions per day: | 15.27544144 |
| mean anomaly at epoch: | 101.9121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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