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212 Explain what is meant by the ascending and descending nodes In what units would these be measured, and in general, would you expect them to change with time 213 Explain what is meant by (a) line of apsides and (b) line of nodes Is it possible for these two lines to be coincident 214 With the aid of a neat sketch, explain what is meant by each of the angles: inclination; argument of perigee; right ascension of the ascending node Which of these angles would you expect, in general, to change with time 215 The inclination of an orbit is 67 What is the greatest latitude, north and south, reached by the subsatellite point Is this orbit retrograde or prograde 216 Describe briefly the main effects of the earth s equatorial bulge on a satellite orbit.

It should be mandatory to perform a full backup of the system right after finishing the installation, since nobody wants to waste two or three days' worth of effort to install the SAP system again. If this is the very first backup, it is a good practice to use the operating system backup utilities or other supported backup software to save the whole server files, including the operating system. Before performing a 81

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Given that a satellite is in a circular equatorial orbit for which the semimajor axis is equal to 42,165 km, calculate (a) the mean motion, (b) the rate of regression of the nodes, and (c) the rate of rotation of argument of perigee 217 A satellite in polar orbit has a perigee height of 600 km and an apogee height of 1200 km Calculate (a) the mean motion, (b) the rate of regression of the nodes, and (c) the rate of rotation of the line of apsides The mean radius of the earth may be assumed equal to 6371 km 218 What is the fundamental unit of universal coordinated time Express the following times in (a) days and (b) degrees: 0 h, 5 min, 24 s; 6 h, 35 min, 20 s; your present time 219.

Determine the Julian days for the following dates and times: midnight March 10, 1999; noon, February 23, 2000; 16:30 h, March 1, 2003; 3 PM, July 4, 2010 220 Find, for the times and dates given in Prob 219, (a) T in Julian centuries and (b) the corresponding GST in degrees 221 Find the month, day, and UT for the following epochs: (a) day 300, year 1999; (b) day 186125, year 2000; (c) day 30012157650, year 2001; (d) day 329441845, year 2004; (e) day 311015, year 2010 222 Find the GST corresponding to the epochs given in Prob 221..

Remote Connection to SAP backup, stop the SAP system to leave it in a consistent state. After you perform this initial backup, you must define a backup strategy including the critical components of the SAP system, such as the database files and the redo logs. This is discussed in detail in Chap. 16.

2.23. The Molnya 3-(25) satellite has the following parameters specified: perigee height 462 km; apogee height 40,850 km; period 736 min; inclination 62.8 . Using an average value of 6371 km for the earth s radius, calculate (a) the semimajor axis and (b) the eccentricity. (c) Calculate the nominal mean motion n0. (d) Calculate the mean motion. (e) Using the calculated value for a, calculate the anomalistic period and compare with the specified value. Calculate (f ) the rate of regression of the nodes, and (g) the rate of rotation of the line of apsides.

225 Determine the orbital condition necessary for the argument of perigee to remain stationary in the orbital plane The orbit for a satellite under this condition has an eccentricity of 0001 and a semimajor axis of 27,000 km At a given epoch the perigee is exactly on the line of Aries Determine the satellite position relative to this line after a period of 30 days from epoch 226 For a given orbit, K as defined by Eq (211) is equal to 0112 rev/day Determine the value of inclination required to make the orbit sun synchronous 227 A satellite has an inclination of 90 and an eccentricity of 01 At epoch, which corresponds to time of perigee passage, the perigee height is 264324 km directly over the north pole Determine (a) the satellite mean motion.

It is also mandatory to make a remote connection to SAP systems as soon as possible. In order to accomplish this, there are some procedures to follow including obtaining the physical connection, the official IP address, and installing and configuring the SAProuter program. Appendix A deals with these topics.

For 1 day after epoch determine (b) the true anomaly, (c) the magnitude of the radius vector to the satellite, and (d) the latitude of the subsatellite point 228 The following elements apply to a satellite in inclined orbit: 0 0 ; w0 90 ; M0 309 ; i 63 ; e 001; a 7130 km An earth station is situated at 45 N, 80 W, and at zero height above sea level Assuming a perfectly spherical earth of uniform mass and radius 6371 km, and given that epoch corresponds to a GST of 116 , determine at epoch the orbital radius vector in the (a) PQW frame; (b) IJK frame; (c) the position vector of the earth station in the IJK frame; (d) the range vector in the IJK frame; (e) the range vector in the SEZ frame; and (f ) the earth station look angles 2.

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