Format: NOD Orbital data as a state vectors, index : 1 Project : INT Satellite: ITP Synomimus: ITZ Launch date : 19950803 ------ TAIL PROBE, INTERBALL PROJECT -----PROJ.launch: 19950803 Inertial coordinate system corresponds to equinox of equator of epoc: J2000 Situation calculation index : 2 Orbit calculation ...
... Data . ... WFPC2 Home . ... WFPC2 History . ... DECON Dates . ... USEAFTER MODE CLK GAIN DATA _FILE S COMMENT 19950112 full off 15 f1k1459eu I for -88њ C, after Jan 13, 1995 decon 19950112 full off 7 f1k1459hu I for -88њ C, after Jan 13, 1995 decon 19950112 full on 15 f1k1459ju I for -88њ C, after Jan 13, 1995 decon 19950112 full on 7 f1k1459nu I for -88њ C, after Jan 13, 1995 decon 19950121 full off 15 f220923ju I for -88њ C, after Jan 13, 1995 decon 19950121 ...