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 67372U 26144.95357256 +.00000000 +00000-0 +87846-4 0 00004
2 67372 97.7999 143.9585 0003736 184.6622 175.4561 14.88250334 07
| Epoch (UTC): | 24 May 2026 22:53:08 |
| Eccentricity: | 0.0003736 |
| inclination: | 97.7999° |
| perigee height: | 601 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 143.9585° |
| argument of perigee: | 184.6622° |
| revolutions per day: | 14.88250334 |
| mean anomaly at epoch: | 175.4561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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