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 26073.55881272 +.00000000 +00000-0 +56340-4 0 00009
2 14373 82.5398 137.9898 0020695 119.8756 240.4520 14.86239288 07
| Epoch (UTC): | 14 March 2026 13:24:41 |
| Eccentricity: | 0.0020695 |
| inclination: | 82.5398° |
| perigee height: | 595 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 137.9898° |
| argument of perigee: | 119.8756° |
| revolutions per day: | 14.86239288 |
| mean anomaly at epoch: | 240.4520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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