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 67329U 26145.02501884 +.00000000 +00000-0 +94478-3 0 00001
2 67329 43.0005 254.1464 0002435 278.6966 81.3610 15.27583562 08
| Epoch (UTC): | 25 May 2026 00:36:01 |
| Eccentricity: | 0.0002435 |
| inclination: | 43.0005° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 254.1464° |
| argument of perigee: | 278.6966° |
| revolutions per day: | 15.27583562 |
| mean anomaly at epoch: | 81.3610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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