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 10143U 26053.49270750 +.00000000 +00000-0 +00000-0 0 00002
2 10143 6.7908 293.4249 0015027 250.0355 320.8155 0.99253520 08
| Epoch (UTC): | 22 February 2026 11:49:29 |
| Eccentricity: | 0.0015027 |
| inclination: | 6.7908° |
| perigee height: | 36011 km |
| apogee height: | 36138 km |
| right ascension of ascending node: | 293.4249° |
| argument of perigee: | 250.0355° |
| revolutions per day: | 0.99253520 |
| mean anomaly at epoch: | 320.8155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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