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 67392U 26145.46838991 +.00000000 +00000-0 +21516-3 0 00004
2 67392 97.4438 144.6714 0007160 61.8314 298.3643 15.18920078 04
| Epoch (UTC): | 25 May 2026 11:14:28 |
| Eccentricity: | 0.0007160 |
| inclination: | 97.4438° |
| perigee height: | 504 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 144.6714° |
| argument of perigee: | 61.8314° |
| revolutions per day: | 15.18920078 |
| mean anomaly at epoch: | 298.3643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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