GET /iss/tle
Get the Two-Line Element (TLE) set for the International Space Station - the standard format used to describe satellite orbits. TLE data includes orbital inclination, eccentricity, argument of perigee, mean motion, and epoch. Used by satellite tracking software (like SGP4 propagators) to predict the ISS position at any future time. Essential for building custom orbital prediction tools and pass-time calculators.
curl https://nordapi.ee/api/v1/iss/tle
{
"data": {
"header": "ISS (ZARYA)",
"id": "25544",
"line1": "1 25544U 98067A 26304.75703384 .00006360 00000+0 12291-3 0 9994",
"line2": "2 25544 51.6332 344.2755 0007028 332.5119 27.5497 15.49131714592920",
"name": "iss",
"requested_timestamp": 1793542964,
"tle_timestamp": 1793470208
},
"success": true
}