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 67451U 26145.35670910 +.00000000 +00000-0 +10732-2 0 00000
2 67451 43.0028 132.5896 0002008 279.6210 80.4414 15.27594011 09
| Epoch (UTC): | 25 May 2026 08:33:39 |
| Eccentricity: | 0.0002008 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.5896° |
| argument of perigee: | 279.6210° |
| revolutions per day: | 15.27594011 |
| mean anomaly at epoch: | 80.4414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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