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 67829U 26145.46822692 +.00000000 +00000-0 +54231-3 0 00000
2 67829 43.0011 193.6797 0001708 278.8598 81.2061 15.27587361 01
| Epoch (UTC): | 25 May 2026 11:14:14 |
| Eccentricity: | 0.0001708 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.6797° |
| argument of perigee: | 278.8598° |
| revolutions per day: | 15.27587361 |
| mean anomaly at epoch: | 81.2061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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