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 14760U 26021.51720828 +.00000000 +00000-0 +17855-3 0 00004
2 14760 74.0431 118.0422 0028777 285.7895 74.0086 14.37146904 06
| Epoch (UTC): | 21 January 2026 12:24:46 |
| Eccentricity: | 0.0028777 |
| inclination: | 74.0431° |
| perigee height: | 747 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 118.0422° |
| argument of perigee: | 285.7895° |
| revolutions per day: | 14.37146904 |
| mean anomaly at epoch: | 74.0086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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