CGRO Cycle 6 Viewing Plan with links to targets


V.P. #Start DateNameZ-axis J2000Z-axis galX-axis J2000OSSE 1OSSE1 J2000OSSE 2OSSE 2 J2000
601.010/29/96 cPSR J2043+2740311.80 26.41 70.06 -10.54236.84 -27.60GRS 1915+105 288.80 10.95NGC 4507 188.90 -39.91
602.011/12/96 aGAL 60+65 220.49 35.76 60.00 65.00264.40 -45.01--- --- ---GAL 353.6+10.7252.28 -28.02
603.011/19/96 aGAL 60+65 220.49 35.76 60.00 65.00269.43 -42.37--- --- ---GAL 356.2+06.4257.90 -28.53
604.011/26/96 aGAL 60+65 220.49 35.76 60.00 65.00280.98 -34.37ARP 220 233.74 23.51GAL 003.7-06.5274.94 -28.91
605.012/03/96 aGAL 60+65 220.49 35.76 60.00 65.00284.16 -31.63ARP 220 233.74 23.51GAL 006.2-10.8280.60 -28.63
606.012/10/96 c3C 279 194.80 -6.45306.41 56.37290.50 -41.293C 279 194.05 -5.79GAL 349.1-06.2266.00 -41.43
607.012/17/96 c3C 279 194.85 -6.39306.52 56.43289.54 -36.133C 279 194.05 -5.79GAL 353.5-03.7266.17 -36.44
608.012/24/96 c3C 279 194.99 -6.14306.79 56.67287.29 -20.473C 279 194.05 -5.79GAL 006.5+03.7266.61 -21.43
609.012/31/96 c3C 279 195.02 -6.03306.86 56.78286.47 -13.463C 279 194.05 -5.79GAL 010.9+06.2266.72 -16.44
610.001/07/97 c3C 279 195.02 -6.04306.86 56.77286.43 -13.093C 279 194.05 -5.79GPLANE 16 274.96 -15.02
611.001/14/97 c3C 279 195.04 -5.97306.89 56.83286.17 -10.663C 279 194.05 -5.79GPLANE 20 276.88 -11.49
612.001/21/97 c3C 279 195.05 -5.90306.92 56.90285.72 -6.433C 279 194.05 -5.79GPLANE 25 279.22 -7.05
613.001/28/97 c3C 279 195.05 -5.83306.94 56.97285.28 -2.233C 279 194.05 -5.79GPLANE 30 281.52 -2.61
614.002/04/97 aVELA 128.83 -45.18263.55 -2.79345.26 -38.65VELA PULSAR 128.83 -45.18NGC 7314 338.94 -26.05
615.002/11/97 cPKS 1622-297 246.52 -29.85348.82 13.32332.00 7.82GPLANE 5 269.27 -24.64CTA 102 338.15 11.73
616.102/18/97 cPKS 0528+134 82.74 13.53191.37 -11.01358.51 -22.67PKS 0528+134 82.74 13.53NGC 7314 338.94 -26.05
616.102/18/97 cPKS 0528+134 82.74 13.53191.37 -11.01358.51 -22.67PKS 0528+134 82.74 13.53NGC 7314 338.94 -26.05
616.703/04/97 cPKS 0528+134 82.74 13.53191.37 -11.01358.51 -22.67PKS 0528+134 82.74 13.53NGC 7314 338.94 -26.05
617.003/18/97 aORION-3 101.60 -8.56220.00 -5.00 14.97 21.323C 120 68.29 5.35PKS 0235+164 39.66 16.62
617.003/18/97 aORION-3 101.60 -8.56220.00 -5.00 14.97 21.323C 120 68.29 5.35PKS 0235+164 39.66 16.62
618.004/12/97 aCARINA-2 139.34 -53.47274.30 -2.95 47.92 -1.05CARINA TANG 146.02 -53.17NGC 4507 188.90 -39.91
619.005/06/97 aCIR X-1 227.77 -59.90319.62 -1.63 76.81 -26.88CIR X-1 230.17 -57.16PSR 1509-58 228.48 -59.13
619.005/06/97 aCIR X-1 227.77 -59.90319.62 -1.63 76.81 -26.88CIR X-1 230.17 -57.16PSR 1509-58 228.48 -59.13
620.006/11/97 aGAL 16+04 271.61 -13.47 15.81 3.59 8.09 -25.23GPLANE 16 274.96 -15.02PKS 2155-304 329.72 -30.23
621.006/17/97 aVELA 131.64 -44.39264.15 -0.73 77.11 30.65VELA PULSAR 128.83 -45.18CRAB PULSAR 83.64 22.01
622.006/24/97 aORION-1 89.05 -21.23226.64 -21.29130.58 62.58ORION GMC 85.50 -1.29NGC 3516 166.68 72.57
623.007/15/97 aORION-2 75.07 -8.18 207.46 -28.40163.58 10.26GPLANE 215 103.80 -1.84NGC 4388 186.45 12.65
624.008/05/97 cGRS 1758-258 266.46 -27.27 1.45 0.83167.83 -16.24GRS 1758-258 270.30 -25.74IC 4329A 207.33 -30.31
625.008/19/97 aGAL 16+00 274.96 -15.02 16.00 0.00192.86 27.13GPLANE 16 274.96 -15.02--- --- ---
626.008/26/97 aGAL 270-75 23.31 -39.31270.03 -75.03148.40 -35.07S ECL POLE 8 4.62 -30.50LMC X-3 84.74 -64.09
627.009/02/97 cPSR 1055-52 164.38 -57.55288.10 2.00165.31 32.44PSR 1055-52 164.49 -52.45NGC 3516 166.68 72.57
628.009/09/97 aGAL 300-74 13.88 -42.80300.16 -74.31146.81 -36.34S ECL POLE 8 4.62 -30.50S ECL POLE 2 84.74 -64.09
629.009/16/97 aGAL 300-74 13.88 -42.80300.16 -74.31153.29 -39.36S ECL POLE 8 4.62 -30.50S ECL POLE 2 84.74 -64.09
630.009/23/97 cPSR 1055-52 164.38 -57.55288.10 2.00165.67 32.44PSR 1055-52 164.49 -52.45NGC 3516 166.68 72.57
631.010/07/97 aVELA 121.50 -44.14259.74 -6.51213.98 -2.56VELA PULSAR 128.83 -45.18NGC 5506 213.31 -3.21
632.010/14/97 aCARINA-1 193.65 -71.05303.19 -8.18198.72 18.88NGC 4945 196.36 -49.47SMC X-1 19.26 -73.44


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 * Z-axis is pointing direction for COMPTEL and EGRET.  OSSE points in X-Z
plane.
  RA and DEC are J2000.
** The reboost dates are subject to change based on orbital parameters.

EGRET Mode:  a = off
             b = fan beam
             c = narrow FOV