AZEL(VI) 6/3/74 AZEL(VI) NAME azel - satellite predictions SYNOPSIS azel [ -d ] [ -l ] satellite1 [ -d ] [ -l ] satellite2 ... DESCRIPTION Azel predicts, in convenient form, the apparent trajectories of Earth satellites whose orbital elements are given in the argument files. If a given satellite name cannot be read, an attempt is made to find it in a directory of satellites maintained by the programs's author. The -d option causes azel to ask for a date and read line 1 data (see below) from the standard input. The -l option causes azel to ask for the observer's latitude, west-longitude, and height above sea level. For each satellite given the program types its full name, the date, and a sequence of lines each containing a time, an azimuth, an elevation, a distance, and a visual magnitude. Each such line indicates that: at the indicated time, the satellite may be seen from Murray Hill (or provided loca- tion) at the indicated azimuth and elevation, and that its distance and apparent magnitude are as given. Predictions are printed only when the sky is dark (sun more than 5 de- grees below the horizon) and when the satellite is not eclipsed by the earth's shadow. Satellites which have not been seen and verified will not have had their visual magni- tude level set correctly. All times input and output by azel are GMT (Universal Time). The satellites for which elements are maintained are: sla,b,e,f,kSkylab A through Skylab K. Skylab A is the labo- ratory; B was the rocket but it has crashed. A and probably K have been verified. cop Copernicus I. Never verified. oao Orbiting Astronomical Observatory. Seen and veri- fied. pag Pageos I. Seen and verified; fairly dim (typical- ly 2nd-3rd magnitude), but elements are extremely accurate. exp19 Explorer 19; seen and verified, but quite dim (4th-5th magnitude) and fast-moving. c103b, c156b, c184b, c206b, c220b, c461b, c500b Various of the USSR Cosmos series; none seen. 7276a Unnamed (satellite # 72-76A); not seen. - 1 - AZEL(VI) 6/3/74 AZEL(VI) The element files used by azel contain five lines. The first line gives a year, month number, day, hour, and minute at which the program begins its consideration of the satel- lite, followed by a number of minutes and an interval in minutes. If the year, month, and day are 0, they are taken to be the current date (taken to change at 6 A.M. local time). The output report starts at the indicated epoch and prints the position of the satellite for the indicated num- ber of minutes at times separated by the indicated interval. This line is ended by two numbers which specify options to the program governing the completeness of the report; they are ordinarily both ``1''. The first option flag suppresses output when the sky is not dark; the second supresses output when the satellite is eclipsed by the earth's shadow. The next line of an element file is the full name of the satel- lite. The next three are the elements themselves (including certain derivatives of the elements). FILES /usr/jfo/el/* - orbital element files SEE ALSO sky(VI) AUTHOR J. F. Ossanna BUGS - 2 -