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 14373U 26074.23206962 +.00000000 +00000-0 +49274-4 0 00000
2 14373 82.5397 137.3581 0020735 117.7759 242.5563 14.86239602 04
| Epoch (UTC): | 15 March 2026 05:34:10 |
| Eccentricity: | 0.0020735 |
| inclination: | 82.5397° |
| perigee height: | 595 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 137.3581° |
| argument of perigee: | 117.7759° |
| revolutions per day: | 14.86239602 |
| mean anomaly at epoch: | 242.5563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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