TruSat / trusat-orbit

Python utilities for processing satellite position observations and managing TLEs

https://trusat.org/about

TruSat/trusat-orbit Issues

Explore move_epoch_to_jd_new() as a mechanism to determine quality of satobs fit
Updated 5 years ago
Create ability to plot value of elements over time
Updated 5 years ago
Create subroutine to identify observation clusters
Updated 5 years ago
Implement weighting for individual IODs for both orbit-fit and rms-reporting
Updated 5 years ago
Create routine to calculate local time of observation
Updated 5 years ago
Add in derived values for ndot and nddot if not obtained from TLE
Updated 5 years ago
Angle parsing should handle Epoch=0 when provided AZ/EL observation
Updated 5 years ago
Implement algorithm to derive approximate orbit number when not provided from TLE
Updated 5 years ago
Add creation of epoch_year and epoch_day variables when initialized from satrec
Updated 5 years ago
iod.parse_iod_line() breaks when seconds are passed the expected boundaries of 0-59
Closed 5 years ago
Setting bstar = 0 does not work
Updated 5 years ago
International Designators are not handled properly with analyst objects
Closed 5 years ago1
TLE formatting issues
Closed 5 years ago6
Legitamate IOD formats are not being accepted
Closed 5 years ago2
IOD regex rejecting seemingly valid entries
Closed 5 years ago1
Restore IOD-file processing workflow in satfit.py:main()
Updated 5 years ago
elfind.py and satid.py depend on v1_4 python-sgp4
Updated 5 years ago
new_rde_data_line_re.search() stalls
Updated 5 years ago2
Angle Regex catches too wide angles
Updated 5 years ago
Finish iod.py:write_uk_line() functionality
Updated 5 years ago