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 10062U 26047.21262449 +.00000000 +00000-0 +24128-3 0 00001
2 10062 28.4166 341.0529 0727050 88.7545 279.6121 13.38952617 03
| Epoch (UTC): | 16 February 2026 05:06:10 |
| Eccentricity: | 0.0727050 |
| inclination: | 28.4166° |
| perigee height: | 569 km |
| apogee height: | 1658 km |
| right ascension of ascending node: | 341.0529° |
| argument of perigee: | 88.7545° |
| revolutions per day: | 13.38952617 |
| mean anomaly at epoch: | 279.6121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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