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 67454U 26145.35028406 +.00000000 +00000-0 +66363-3 0 00002
2 67454 43.0030 132.5449 0002016 281.2248 78.8377 15.27596230 02
| Epoch (UTC): | 25 May 2026 08:24:24 |
| Eccentricity: | 0.0002016 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.5449° |
| argument of perigee: | 281.2248° |
| revolutions per day: | 15.27596230 |
| mean anomaly at epoch: | 78.8377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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