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 26076.18451271 +.00000000 +00000-0 +45578-4 0 00004
2 14373 82.5392 135.5259 0020818 111.7247 248.6189 14.86241261 04
| Epoch (UTC): | 17 March 2026 04:25:41 |
| Eccentricity: | 0.0020818 |
| inclination: | 82.5392° |
| perigee height: | 595 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 135.5259° |
| argument of perigee: | 111.7247° |
| revolutions per day: | 14.86241261 |
| mean anomaly at epoch: | 248.6189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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