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 14328U 26150.61757897 +.00000000 +00000-0 +00000-0 0 00005
2 14328 14.3238 346.0645 0016211 73.8866 284.8937 0.99408342 08
| Epoch (UTC): | 30 May 2026 14:49:18 |
| Eccentricity: | 0.0016211 |
| inclination: | 14.3238° |
| perigee height: | 35962 km |
| apogee height: | 36099 km |
| right ascension of ascending node: | 346.0645° |
| argument of perigee: | 73.8866° |
| revolutions per day: | 0.99408342 |
| mean anomaly at epoch: | 284.8937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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