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 67234U 26144.97337784 +.00000000 +00000-0 +23863-4 0 00006
2 67234 97.9648 152.5949 0001332 77.1073 283.0285 14.75876797 05
| Epoch (UTC): | 24 May 2026 23:21:39 |
| Eccentricity: | 0.0001332 |
| inclination: | 97.9648° |
| perigee height: | 641 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 152.5949° |
| argument of perigee: | 77.1073° |
| revolutions per day: | 14.75876797 |
| mean anomaly at epoch: | 283.0285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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