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 67386U 26145.45383711 +.00000000 +00000-0 +17211-3 0 00008
2 67386 97.7997 144.5341 0002634 163.5172 196.6131 14.88743256 07
| Epoch (UTC): | 25 May 2026 10:53:31 |
| Eccentricity: | 0.0002634 |
| inclination: | 97.7997° |
| perigee height: | 600 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 144.5341° |
| argument of perigee: | 163.5172° |
| revolutions per day: | 14.88743256 |
| mean anomaly at epoch: | 196.6131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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