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 66767U 26145.15621647 +.00000000 +00000-0 +15842-3 0 00008
2 66767 97.4166 219.1544 0001105 104.4677 255.6681 15.19780591 08
| Epoch (UTC): | 25 May 2026 03:44:57 |
| Eccentricity: | 0.0001105 |
| inclination: | 97.4166° |
| perigee height: | 506 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 219.1544° |
| argument of perigee: | 104.4677° |
| revolutions per day: | 15.19780591 |
| mean anomaly at epoch: | 255.6681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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