Astronomy
解析 TLE、显示开普勒轨道根数(含半长轴/周期推导)、SGP4 传播求 ECI/地面轨迹/星下点、仰角可见性、多普勒频移
用三种语言从你的代码中调用此工具。
curl -X POST 'https://api.elysiatools.com/zh/api/tools/keplerian-orbital-element-tle-satrec-position' \
-H 'Content-Type: application/json' \
-d '{"line1":"1 25544U 98067A 25220.50000000 .00000000 00000-0 00000-0 0 9996","line2":"2 25544 51.6400 200.0000 0001000 90.0000 270.0000 15.50000000123455","propTime":"","observerLat":0,"observerLon":0,"txFreqMHz":0,"trackSamples":60}'以 JSON 形式 POST 提交输入参数。文件类型参数需先单独上传。
POST https://api.elysiatools.com/zh/api/tools/keplerian-orbital-element-tle-satrec-position| 参数名 | 类型 | 必填 | 说明 |
|---|---|---|---|
| line1 | textarea | 是 | — |
| line2 | textarea | 是 | — |
| propTime | text | 否 | — |
| observerLat | number | 否 | — |
| observerLon | number | 否 | — |
| txFreqMHz | number |
将此工具加入你的 Model Context Protocol 服务,让 AI 智能体可以列出并调用它。
将以下内容加入你的 MCP 客户端配置:
{
"mcpServers": {
"elysiatools-keplerian-orbital-element-tle-satrec-position": {
"name": "keplerian-orbital-element-tle-satrec-position",
"description": "解析 TLE、显示开普勒轨道根数(含半长轴/周期推导)、SGP4 传播求 ECI/地面轨迹/星下点、仰角可见性、多普勒频移",
"baseUrl": "https://api.elysiatools.com/mcp/sse?toolId=keplerian-orbital-element-tle-satrec-position",
"command": "",
"args": [],
"env": {},
"isActive": true,
"type": "sse"
}
}
}连接到 SSE 端点后,列出已开放的工具:
{
"jsonrpc": "2.0",
"id": 1,
"method": "tools/list"
}通过工具 id 调用,参数由其参数表构建:
{
"jsonrpc": "2.0",
"id": 2,
"method": "tools/call",
"params": {
"name": "keplerian-orbital-element-tle-satrec-position",
"arguments": {
"line1": "1 25544U 98067A 25220.50000000 .00000000 00000-0 00000-0 0 9996",
"line2": "2 25544 51.6400 200.0000 0001000 90.0000 270.0000 15.50000000123455",
"propTime": "",
"observerLat": 0,
"observerLon": 0,
"txFreqMHz": 0,
"trackSamples": 60
}
}
}有问题或反馈?请联系 [email protected]
| 否 |
| — |
| trackSamples | number | 否 | — |
HTML 结果
{
"result": "<div>Processed HTML content</div>",
"error": "Error message (optional)",
"message": "Notification message (optional)",
"metadata": {
"key": "value"
}
}