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 67465U 26145.37969139 +.00000000 +00000-0 +36562-3 0 00001
2 67465 42.9993 131.8787 0002045 283.0990 76.9633 15.27570353 05
| Epoch (UTC): | 25 May 2026 09:06:45 |
| Eccentricity: | 0.0002045 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.8787° |
| argument of perigee: | 283.0990° |
| revolutions per day: | 15.27570353 |
| mean anomaly at epoch: | 76.9633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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