Main differences between V7.2 and V7.2.1

Non obfuscated methods

• the LEOManIncInfo.getInc() method is now available (no more obfuscated)

Additional output information

• Adding information on the object

 Name			: DELTA 1 DEB
 Country		: US
 Hper			: 234.02019063088298 km
 Hapo			: 261.37029874148595 km
 Incl			: 29.0708 deg

• Adding the margin on the reentry date as below:

 Re-entry date 		: 2011-11-30T15:37:29.221
 Re-entry date error 	: +/-10.6 days

• When Orbit Determination (OD) is not successful, reentry date (and margin on it) using the refined S/m is still displayed
• Adding units on S/m results:

 SmDragApriori 	: 0.05916134793505359 kg/m2
 SmDragRefined 	: 0.05457889062590913 kg/m2
 SmDragAfterOD 	: 0.050351376463313384 kg/m2
 SmSRPRefined 	: 0.0 kg/m2

• Changing type of font for better readibility.

Anomaly corrections

• When the computation exits in error mode due to the OperaException type (typically if there is a problem when reading TLE), the management of such exception allows now going on computation for next Norad Ids.
• OPERA does correctly take into account PATRIUS_DATASET and the Opera configuration file for some batch configurations (for Search by Sat or Search by Orb options).
• The Opera configuration file (including all the by default configurations) is now correctly read if the name of a directory will start by "/".
• No more erroneous error messages between BYSAT et BYORB.
• No more error on the reentry date margin when the computation is executed from the GUII (previously divided by 100).