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What's a Two Line Element Set (TLE)? A two line element set (TLE) is a group of numbers provided in two lines and separated by spaces, that specify the orbital parameters (elements) for a satellite, spent booster rocket, or other man-made satellites. A Typical TLE, and what the numbers are: ISS (ZARYA) 1 25544U 98067A 02166.25000000 .00022749 00000-0 30765-3 0 5637 2 25544 51.6332 62.6174 0006804 238.6710 31.2451 15.57611327203721 NAME 1 [IDXXXU] [Int Desig] [Epoch] [FTD MM] [STD MM] [drag] [Eph T] [Ele #] 2 [IDXXXX] [Inc] [RA AN] [Ecc] [AOP] [MA] [Revs]+[ON] Note: Not all these numbers are needed for programming your Autostar manually. Downloadable TLE's can be imported into the Autostar using the Meade #505 cable or equivalent, and the Autostar update software. TLE Name ISS (Zarya) - International Space Station, (Zarya Module) Line One ID = Satellite Number - 25544U (U=unclassified) Int Desig = International Designation (date lauched, launch number of year, section) - 98067A Epoch = Year (last two digits) , day of year, and fractional day - 2002, day 166.25000000 FTD MM= First Time Derivative of Mean Motion - .00022749 STD MM= Second Time Derivative of Mean Motion - 00000-0 drag = BSTAR drag term (decimal assumed) - 30765-3 Eph T = Ephemeris Type - 0 Ele # = Element Number - 5637 Line Two ID = Satellite Number - 25544 Inc = Inclination (degrees) - 51.6332 RA AN = Right Ascension of Ascending Node (degrees) - 62.6174 Ecc = Eccentricity (decimal assumed) - .0006804 AOP = Argument of Perigree (degrees) - 238.6710 MA = Mean Anomaly (degrees) - 31.2451 Revs = Revolutions per day - 15.57611327 ON = Orbit Number at Epoch - 20372(.)1 What's "AOS"?
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