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 26075.61689367 +.00000000 +00000-0 +47314-3 0 00009
2 43803 97.4246 138.2940 0005146 227.0437 133.0373 15.30577082 08
| Epoch (UTC): | 16 March 2026 14:48:19 |
| Eccentricity: | 0.0005146 |
| inclination: | 97.4246° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 138.2940° |
| argument of perigee: | 227.0437° |
| revolutions per day: | 15.30577082 |
| mean anomaly at epoch: | 133.0373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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