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 67045U 26145.50450700 +.00000000 +00000-0 +11057-2 0 00000
2 67045 43.0007 324.5560 0002010 268.4805 91.5817 15.27594721 03
| Epoch (UTC): | 25 May 2026 12:06:29 |
| Eccentricity: | 0.0002010 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.5560° |
| argument of perigee: | 268.4805° |
| revolutions per day: | 15.27594721 |
| mean anomaly at epoch: | 91.5817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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