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 67160U 26141.82666014 +.00000000 +00000-0 +00000-0 0 00000
2 67160 54.3194 102.8809 0001476 247.4028 291.0151 1.70474125 01
| Epoch (UTC): | 21 May 2026 19:50:23 |
| Eccentricity: | 0.0001476 |
| inclination: | 54.3194° |
| perigee height: | 23218 km |
| apogee height: | 23227 km |
| right ascension of ascending node: | 102.8809° |
| argument of perigee: | 247.4028° |
| revolutions per day: | 1.70474125 |
| mean anomaly at epoch: | 291.0151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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