Table 3
Minimum and Maximum RM magnitudes for different orbit altitudes when the TOF Leg 1 is from 4.0 to 6.0 hour and the TOF Leg 2 is from 5.0 to 5.5 days

Recovered circular orbit altitude (km)	RM #1 Mag. (km/s)		RM #2 Mag. (km/s)		RM #1 + RM #2 Mag. (km/s)
	Min.	Max.	Min.	Max.	Min.	Max.
	30	0.612	0.694	0.787	0.824	1.398	1.519
50	0.612	0.695	0.779	0.817	1.392	1.513
100	0.613	0.695	0.764	0.802	1.377	1.498
200	0.615	0.697	0.734	0.773	1.350	1.470
500	0.621	0.701	0.660	0.699	1.181	1.400
1,000	0.625	0.708	0.565	0.603	1.190	1.312