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 67145U 26145.58335647 +.00000000 +00000-0 -14916+0 0 00006
2 67145 51.8954 66.2998 0001727 334.8324 295.7094 15.00648200 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001727 |
| inclination: | 51.8954° |
| perigee height: | 564 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 66.2998° |
| argument of perigee: | 334.8324° |
| revolutions per day: | 15.00648200 |
| mean anomaly at epoch: | 295.7094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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