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 26275.85265373 .00005805 00000+0 11452-3 0 9994",
"line2": "2 25544 51.6313 127.2636 0006924 216.0999 143.9522 15.48720404588445",
"name": "iss",
"requested_timestamp": 1791066685,
"tle_timestamp": 1790972869
},
"success": true
}