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 67324U 26145.60193654 +.00000000 +00000-0 +50482-3 0 00009
2 67324 42.9977 250.7321 0001881 265.8808 94.1829 15.27576904 06
| Epoch (UTC): | 25 May 2026 14:26:47 |
| Eccentricity: | 0.0001881 |
| inclination: | 42.9977° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.7321° |
| argument of perigee: | 265.8808° |
| revolutions per day: | 15.27576904 |
| mean anomaly at epoch: | 94.1829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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