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 14234U 26149.22533536 +.00000000 +00000-0 +00000-0 0 00008
2 14234 13.7976 342.1214 0024322 169.9311 190.0676 0.99527344 01
| Epoch (UTC): | 29 May 2026 05:24:28 |
| Eccentricity: | 0.0024322 |
| inclination: | 13.7976° |
| perigee height: | 35894 km |
| apogee height: | 36100 km |
| right ascension of ascending node: | 342.1214° |
| argument of perigee: | 169.9311° |
| revolutions per day: | 0.99527344 |
| mean anomaly at epoch: | 190.0676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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