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 67335U 26145.36799883 +.00000000 +00000-0 +57957-3 0 00004
2 67335 43.0017 153.7854 0001751 268.9615 91.1036 15.27595785 09
| Epoch (UTC): | 25 May 2026 08:49:55 |
| Eccentricity: | 0.0001751 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.7854° |
| argument of perigee: | 268.9615° |
| revolutions per day: | 15.27595785 |
| mean anomaly at epoch: | 91.1036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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