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 67228U 26144.98337468 +.00000000 +00000-0 +32338-3 0 00005
2 67228 42.0081 355.3023 0010427 211.1453 148.8755 14.98768799 00
| Epoch (UTC): | 24 May 2026 23:36:03 |
| Eccentricity: | 0.0010427 |
| inclination: | 42.0081° |
| perigee height: | 563 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 355.3023° |
| argument of perigee: | 211.1453° |
| revolutions per day: | 14.98768799 |
| mean anomaly at epoch: | 148.8755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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