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 67832U 26145.58452169 +.00000000 +00000-0 +64168-3 0 00005
2 67832 43.0002 185.7647 0001215 272.1262 87.9450 15.27599316 07
| Epoch (UTC): | 25 May 2026 14:01:42 |
| Eccentricity: | 0.0001215 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.7647° |
| argument of perigee: | 272.1262° |
| revolutions per day: | 15.27599316 |
| mean anomaly at epoch: | 87.9450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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