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 43803U 26069.73254389 +.00000000 +00000-0 +70573-3 0 00000
2 43803 97.4246 132.4087 0004801 252.6342 107.4374 15.30348491 08
| Epoch (UTC): | 10 March 2026 17:34:51 |
| Eccentricity: | 0.0004801 |
| inclination: | 97.4246° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 132.4087° |
| argument of perigee: | 252.6342° |
| revolutions per day: | 15.30348491 |
| mean anomaly at epoch: | 107.4374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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