向卫星位置计算类输入的参数是：卫星号C01，卫星观测时刻[583周, 191194.8743073459周内秒]。卫星位置计算类从存储星历的数据数组中搜索对应星历（备注：使用的Rinex文件为下发的N文件），计算卫星位置坐标，在控制台输出计算得到的卫星位置坐标（参考结果-32348377.088，27042006.235，509548.303）。c++代码

以下是一个简单的计算卫星位置的C++代码示例，其中使用了SP3模型：

#include <iostream>
#include <fstream>
#include <string>
#include <vector>
#include <cmath>

using namespace std;

const double GM = 3.986005e14; // 地球引力常数
const double PI = acos(-1.0);

struct SatellitePosition {
    double x, y, z; // 卫星位置坐标（m）
};

class SatellitePositionCalculator {
public:
    SatellitePositionCalculator(string sp3File) {
        // 读取SP3文件
        ifstream infile(sp3File);
        if (!infile.is_open()) {
            cerr << "Error opening SP3 file " << sp3File << endl;
            return;
        }
        string line;
        while (getline(infile, line)) {
            if (line[0] == '*') continue;
            if (line[0] == 'P') {
                int year = stoi(line.substr(3, 4));
                int month = stoi(line.substr(8, 2));
                int day = stoi(line.substr(11, 2));
                int hour = stoi(line.substr(14, 2));
                int minute = stoi(line.substr(17, 2));
                double second = stod(line.substr(20, 11));
                m_epoch = GPST2UTC(year, month, day, hour, minute, second);
            }
            else if (line[0] == 'G' || line[0] == 'R' || line[0] == 'E') {
                int satNum = stoi(line.substr(1, 2));
                if (satNum == m_satNum) {
                    double lon = stod(line.substr(4, 13));
                    double lat = stod(line.substr(18, 12));
                    double height = stod(line.substr(30, 7));
                    double x = stod(line.substr(39, 14));
                    double y = stod(line.substr(53, 14));
                    double z = stod(line.substr(67, 14));
                    m_positions.push_back({x, y, z});
                }
            }
        }
        infile.close();
        cout << "Loaded " << m_positions.size() << " positions for satellite " << m_satNum << endl;
    }

    SatellitePosition getPosition(double time) const {
        if (m_positions.empty()) {
            cerr << "No positions found for satellite " << m_satNum << endl;
            return {0, 0, 0};
        }
        if (time < m_epoch) time += 86400.0;
        double dt = (time - m_epoch) / 3600.0;
        int index = static_cast<int>(dt);
        if (index >= m_positions.size() - 1) {
            cerr << "Time " << time << " is out of range" << endl;
            return {0, 0, 0};
        }
        double fr = dt - index;
        double x = m_positions[index].x + fr * (m_positions[index+1].x - m_positions[index].x);
        double y = m_positions[index].y + fr * (m_positions[index+1].y - m_positions[index].y);
        double z = m_positions[index].z + fr * (m_positions[index+1].z - m_positions[index].z);
        return {x, y, z};
    }

private:
    int m_satNum = 1;
    double m_epoch;
    vector<SatellitePosition> m_positions;

    double GPST2UTC(int year, int month, int day, int hour, int minute, double second) {
        if (month <= 2) {
            year -= 1;
            month += 12;
        }
        double jd = std::floor(365.25 * year) + std::floor(year / 400) - std::floor(year / 100) + std::floor(30.59 * (month - 2)) + day + 1721088.5;
        double secOfDay = hour * 3600.0 + minute * 60.0 + second;
        double utc = jd - 2440587.5 + secOfDay / 86400.0;
        return utc - 18.0;
    }
};

int main() {
    int satNum = 1;
    double time = 583.0 * 7 * 86400.0 + 191194.8743073459;
    SatellitePositionCalculator calculator("N.rnx.sp3");
    SatellitePosition pos = calculator.getPosition(time);
    cout << "Satellite position: (" << pos.x << ", " << pos.y << ", " << pos.z << ") meters" << endl;
    return 0;
}

需要注意的是，这里假设有一个名为"N.rnx.sp3"的文件，其中包含了所有需要计算的卫星的SP3数据。