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 67020U 26145.56921939 +.00000000 +00000-0 +41531-3 0 00007
2 67020 70.0006 260.6107 0002847 274.2522 85.8312 14.98325105 02
| Epoch (UTC): | 25 May 2026 13:39:40 |
| Eccentricity: | 0.0002847 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.6107° |
| argument of perigee: | 274.2522° |
| revolutions per day: | 14.98325105 |
| mean anomaly at epoch: | 85.8312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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