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 26064.26783115 +.00000000 +00000-0 +78510-4 0 00007
2 14373 82.5412 146.7066 0020148 148.9376 211.3037 14.86228515 04
| Epoch (UTC): | 05 March 2026 06:25:40 |
| Eccentricity: | 0.0020148 |
| inclination: | 82.5412° |
| perigee height: | 596 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 146.7066° |
| argument of perigee: | 148.9376° |
| revolutions per day: | 14.86228515 |
| mean anomaly at epoch: | 211.3037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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