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 67393U 26145.46826647 +.00000000 +00000-0 +21463-3 0 00001
2 67393 97.4583 144.9984 0007127 65.3534 294.8442 15.18920467 04
| Epoch (UTC): | 25 May 2026 11:14:18 |
| Eccentricity: | 0.0007127 |
| inclination: | 97.4583° |
| perigee height: | 504 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 144.9984° |
| argument of perigee: | 65.3534° |
| revolutions per day: | 15.18920467 |
| mean anomaly at epoch: | 294.8442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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