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 10144U 26071.45888384 +.00000000 +00000-0 +39229-3 0 00005
2 10144 29.0634 117.2670 0840402 225.0464 127.8879 13.25859360 05
| Epoch (UTC): | 12 March 2026 11:00:47 |
| Eccentricity: | 0.0840402 |
| inclination: | 29.0634° |
| perigee height: | 529 km |
| apogee height: | 1796 km |
| right ascension of ascending node: | 117.2670° |
| argument of perigee: | 225.0464° |
| revolutions per day: | 13.25859360 |
| mean anomaly at epoch: | 127.8879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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