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 06153U 26018.96802501 +.00000000 +00000-0 +61614-4 0 00008
2 06153 35.0040 220.5898 0005932 116.4921 41.1857 14.59943757 06
| Epoch (UTC): | 18 January 2026 23:13:57 |
| Eccentricity: | 0.0005932 |
| inclination: | 35.0040° |
| perigee height: | 689 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 220.5898° |
| argument of perigee: | 116.4921° |
| revolutions per day: | 14.59943757 |
| mean anomaly at epoch: | 41.1857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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