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 67276U 26145.15059794 +.00000000 +00000-0 +30352-3 0 00005
2 67276 97.3910 220.0660 0015476 89.8796 270.4214 15.22307891 03
| Epoch (UTC): | 25 May 2026 03:36:51 |
| Eccentricity: | 0.0015476 |
| inclination: | 97.3910° |
| perigee height: | 488 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 220.0660° |
| argument of perigee: | 89.8796° |
| revolutions per day: | 15.22307891 |
| mean anomaly at epoch: | 270.4214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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