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 67986U 26145.54930280 +.00000000 +00000-0 +77206-3 0 00003
2 67986 42.9978 335.2589 0000447 262.9946 97.0855 15.27596437 08
| Epoch (UTC): | 25 May 2026 13:10:59 |
| Eccentricity: | 0.0000447 |
| inclination: | 42.9978° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 335.2589° |
| argument of perigee: | 262.9946° |
| revolutions per day: | 15.27596437 |
| mean anomaly at epoch: | 97.0855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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