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 67467U 26145.02463691 +.00000000 +00000-0 +37627-3 0 00000
2 67467 43.0014 134.3953 0001354 272.2593 87.8104 15.27592358 00
| Epoch (UTC): | 25 May 2026 00:35:28 |
| Eccentricity: | 0.0001354 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 134.3953° |
| argument of perigee: | 272.2593° |
| revolutions per day: | 15.27592358 |
| mean anomaly at epoch: | 87.8104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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