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 26073.59016574 +.00000000 +00000-0 +83935-3 0 00007
2 43803 97.4249 136.2668 0004997 235.6318 124.4451 15.30507754 02
| Epoch (UTC): | 14 March 2026 14:09:50 |
| Eccentricity: | 0.0004997 |
| inclination: | 97.4249° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 136.2668° |
| argument of perigee: | 235.6318° |
| revolutions per day: | 15.30507754 |
| mean anomaly at epoch: | 124.4451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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