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 26064.60446236 +.00000000 +00000-0 +78987-4 0 00003
2 14373 82.5412 146.3908 0020170 147.8715 212.3736 14.86228943 07
| Epoch (UTC): | 05 March 2026 14:30:25 |
| Eccentricity: | 0.0020170 |
| inclination: | 82.5412° |
| perigee height: | 596 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 146.3908° |
| argument of perigee: | 147.8715° |
| revolutions per day: | 14.86228943 |
| mean anomaly at epoch: | 212.3736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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