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 26159.20594875 +.00000000 +00000-0 +77721-4 0 00006
2 13242 74.0430 94.8896 0025159 212.2879 147.6736 14.37393174 05
| Epoch (UTC): | 08 June 2026 04:56:33 |
| Eccentricity: | 0.0025159 |
| inclination: | 74.0430° |
| perigee height: | 749 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 94.8896° |
| argument of perigee: | 212.2879° |
| revolutions per day: | 14.37393174 |
| mean anomaly at epoch: | 147.6736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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