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 67056U 26145.47237913 +.00000000 +00000-0 +67670-3 0 00000
2 67056 43.0021 324.3162 0000781 276.7970 83.2792 15.27588522 07
| Epoch (UTC): | 25 May 2026 11:20:13 |
| Eccentricity: | 0.0000781 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.3162° |
| argument of perigee: | 276.7970° |
| revolutions per day: | 15.27588522 |
| mean anomaly at epoch: | 83.2792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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