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 67162U 26143.59011919 +.00000000 +00000-0 +00000-0 0 00006
2 67162 54.3227 102.8298 0003475 303.3884 57.4130 1.70474193 01
| Epoch (UTC): | 23 May 2026 14:09:46 |
| Eccentricity: | 0.0003475 |
| inclination: | 54.3227° |
| perigee height: | 23212 km |
| apogee height: | 23232 km |
| right ascension of ascending node: | 102.8298° |
| argument of perigee: | 303.3884° |
| revolutions per day: | 1.70474193 |
| mean anomaly at epoch: | 57.4130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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