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 11427U 26088.15765765 +.00000000 +00000-0 +89599-4 0 00008
2 11427 74.0153 236.3132 0020157 325.8810 34.1047 14.38853086 04
| Epoch (UTC): | 29 March 2026 03:47:01 |
| Eccentricity: | 0.0020157 |
| inclination: | 74.0153° |
| perigee height: | 748 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 236.3132° |
| argument of perigee: | 325.8810° |
| revolutions per day: | 14.38853086 |
| mean anomaly at epoch: | 34.1047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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