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 67429U 26145.35896465 +.00000000 +00000-0 +61287-3 0 00002
2 67429 43.0006 164.8531 0001519 266.8322 93.2356 15.27583927 03
| Epoch (UTC): | 25 May 2026 08:36:54 |
| Eccentricity: | 0.0001519 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.8531° |
| argument of perigee: | 266.8322° |
| revolutions per day: | 15.27583927 |
| mean anomaly at epoch: | 93.2356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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