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 67272U 26145.15101588 +.00000000 +00000-0 +47103-3 0 00002
2 67272 97.3942 220.2748 0015650 87.4334 272.8694 15.23590729 02
| Epoch (UTC): | 25 May 2026 03:37:27 |
| Eccentricity: | 0.0015650 |
| inclination: | 97.3942° |
| perigee height: | 484 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 220.2748° |
| argument of perigee: | 87.4334° |
| revolutions per day: | 15.23590729 |
| mean anomaly at epoch: | 272.8694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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