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 67350U 26145.36929659 +.00000000 +00000-0 +67252-3 0 00006
2 67350 43.0012 153.7926 0001815 257.3485 102.7164 15.27570092 04
| Epoch (UTC): | 25 May 2026 08:51:47 |
| Eccentricity: | 0.0001815 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.7926° |
| argument of perigee: | 257.3485° |
| revolutions per day: | 15.27570092 |
| mean anomaly at epoch: | 102.7164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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