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 26065.47970316 +.00000000 +00000-0 +76647-4 0 00001
2 14373 82.5412 145.5698 0020205 145.1611 215.0933 14.86229865 02
| Epoch (UTC): | 06 March 2026 11:30:46 |
| Eccentricity: | 0.0020205 |
| inclination: | 82.5412° |
| perigee height: | 596 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 145.5698° |
| argument of perigee: | 145.1611° |
| revolutions per day: | 14.86229865 |
| mean anomaly at epoch: | 215.0933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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