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 67355U 26145.34758463 +.00000000 +00000-0 +46975-3 0 00001
2 67355 43.0035 154.5031 0001640 268.3909 91.6755 15.27594052 03
| Epoch (UTC): | 25 May 2026 08:20:31 |
| Eccentricity: | 0.0001640 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.5031° |
| argument of perigee: | 268.3909° |
| revolutions per day: | 15.27594052 |
| mean anomaly at epoch: | 91.6755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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