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.