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 67358U 26145.30005821 +.00000000 +00000-0 +55018-3 0 00001
2 67358 42.9990 154.1303 0000768 273.4945 86.5819 15.27605651 01
| Epoch (UTC): | 25 May 2026 07:12:05 |
| Eccentricity: | 0.0000768 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 154.1303° |
| argument of perigee: | 273.4945° |
| revolutions per day: | 15.27605651 |
| mean anomaly at epoch: | 86.5819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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