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 67345U 26145.30647015 +.00000000 +00000-0 +62770-3 0 00007
2 67345 43.0002 154.1848 0001252 261.4991 98.5719 15.27586044 00
| Epoch (UTC): | 25 May 2026 07:21:19 |
| Eccentricity: | 0.0001252 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.1848° |
| argument of perigee: | 261.4991° |
| revolutions per day: | 15.27586044 |
| mean anomaly at epoch: | 98.5719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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