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 67449U 26145.01564177 +.00000000 +00000-0 +61718-3 0 00008
2 67449 42.9964 134.3139 0000807 259.6949 100.3812 15.27593692 03
| Epoch (UTC): | 25 May 2026 00:22:31 |
| Eccentricity: | 0.0000807 |
| inclination: | 42.9964° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 134.3139° |
| argument of perigee: | 259.6949° |
| revolutions per day: | 15.27593692 |
| mean anomaly at epoch: | 100.3812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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