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 26071.67369220 +.00000000 +00000-0 +60539-4 0 00009
2 14373 82.5401 139.7586 0020599 125.6936 234.6202 14.86237354 08
| Epoch (UTC): | 12 March 2026 16:10:07 |
| Eccentricity: | 0.0020599 |
| inclination: | 82.5401° |
| perigee height: | 595 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 139.7586° |
| argument of perigee: | 125.6936° |
| revolutions per day: | 14.86237354 |
| mean anomaly at epoch: | 234.6202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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