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 26106.86391193 +.00000000 +00000-0 +00000-0 0 00007
2 10143 6.6637 292.9964 0014911 245.9444 315.2646 0.99253062 01
| Epoch (UTC): | 16 April 2026 20:44:01 |
| Eccentricity: | 0.0014911 |
| inclination: | 6.6637° |
| perigee height: | 36011 km |
| apogee height: | 36138 km |
| right ascension of ascending node: | 292.9964° |
| argument of perigee: | 245.9444° |
| revolutions per day: | 0.99253062 |
| mean anomaly at epoch: | 315.2646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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