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 67334U 26145.32447267 +.00000000 +00000-0 +83393-3 0 00008
2 67334 43.0040 154.3267 0000540 224.2057 135.8752 15.27609088 02
| Epoch (UTC): | 25 May 2026 07:47:14 |
| Eccentricity: | 0.0000540 |
| inclination: | 43.0040° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 154.3267° |
| argument of perigee: | 224.2057° |
| revolutions per day: | 15.27609088 |
| mean anomaly at epoch: | 135.8752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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