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 26073.91706389 +.00000000 +00000-0 +77318-3 0 00001
2 43803 97.4249 136.5939 0005016 233.9702 126.1074 15.30521716 01
| Epoch (UTC): | 14 March 2026 22:00:34 |
| Eccentricity: | 0.0005016 |
| inclination: | 97.4249° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 136.5939° |
| argument of perigee: | 233.9702° |
| revolutions per day: | 15.30521716 |
| mean anomaly at epoch: | 126.1074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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