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 26065.28295906 +.00000000 +00000-0 +12455-3 0 00008
2 11427 74.0144 278.5570 0019219 13.1178 347.0472 14.38839939 08
| Epoch (UTC): | 06 March 2026 06:47:27 |
| Eccentricity: | 0.0019219 |
| inclination: | 74.0144° |
| perigee height: | 749 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 278.5570° |
| argument of perigee: | 13.1178° |
| revolutions per day: | 14.38839939 |
| mean anomaly at epoch: | 347.0472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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