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 13242U 26074.22523825 +.00000000 +00000-0 +66232-4 0 00006
2 13242 74.0409 251.1746 0023982 25.3519 334.8805 14.37355051 08
| Epoch (UTC): | 15 March 2026 05:24:20 |
| Eccentricity: | 0.0023982 |
| inclination: | 74.0409° |
| perigee height: | 750 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 251.1746° |
| argument of perigee: | 25.3519° |
| revolutions per day: | 14.37355051 |
| mean anomaly at epoch: | 334.8805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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