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 67076U 26145.50987964 +.00000000 +00000-0 +28307-3 0 00008
2 67076 70.0012 180.7910 0003731 267.4947 92.5785 14.98336880 03
| Epoch (UTC): | 25 May 2026 12:14:13 |
| Eccentricity: | 0.0003731 |
| inclination: | 70.0012° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.7910° |
| argument of perigee: | 267.4947° |
| revolutions per day: | 14.98336880 |
| mean anomaly at epoch: | 92.5785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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