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 14134U 26100.84457500 +.00000000 +00000-0 +00000-0 0 00008
2 14134 11.6727 329.9525 0002374 69.9521 129.2182 1.00173889 04
| Epoch (UTC): | 10 April 2026 20:16:11 |
| Eccentricity: | 0.0002374 |
| inclination: | 11.6727° |
| perigee height: | 35804 km |
| apogee height: | 35824 km |
| right ascension of ascending node: | 329.9525° |
| argument of perigee: | 69.9521° |
| revolutions per day: | 1.00173889 |
| mean anomaly at epoch: | 129.2182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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