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 67351U 26145.36157566 +.00000000 +00000-0 +36517-3 0 00007
2 67351 42.9994 153.7323 0001733 264.4323 95.6331 15.27584100 03
| Epoch (UTC): | 25 May 2026 08:40:40 |
| Eccentricity: | 0.0001733 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.7323° |
| argument of perigee: | 264.4323° |
| revolutions per day: | 15.27584100 |
| mean anomaly at epoch: | 95.6331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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