Issues
- 0
Report an error:JplError: No frame loaded
#42 opened by yangyang-studio - 2
Latest error: ValueError: Unknown 'TLS'
#39 opened by yangyang-studio - 3
LTAN calculation
#41 opened by karatemir - 3
- 1
KeyError: 'Earth'
#38 opened by yangyang-studio - 2
Collaborate and share low level code
#36 opened by astrojuanlu - 0
Slow GCRF conversion
#35 opened by galactics - 1
- 1
Retrieval of frame transformation matrix
#6 opened by galactics - 0
New propagators
#7 opened by galactics - 0
Forgotten statevector replacement
#32 opened by galactics - 0
Separation between state-vector and orbit
#10 opened by galactics - 0
Change frame handling
#5 opened by galactics - 3
J2 analytic propagator
#31 opened by rodrigo-moliveira - 2
Allow for hyperbolic keplerian form
#27 opened by galactics - 0
Argument of latitude
#30 opened by galactics - 0
variable step size for Listeners
#29 opened by galactics - 0
atmospheric drag
#28 opened by galactics - 0
Timescales as timezones
#25 opened by galactics - 0
Leap-second handling as per PEP495
#26 opened by galactics - 0
Tropospheric delay
#23 opened by galactics - 0
Conditionnal Maneuver
#24 opened by galactics - 0
- 0
Use annotations
#19 opened by galactics - 0
Node2 simplification
#16 opened by galactics - 0
Lagrange interpolation in ephemeris
#15 opened by galactics - 0
mention licence in the readme
#22 opened by galactics - 0
bisect method reimplementation
#21 opened by galactics - 0
Keplerian form should depend on central body
#20 opened by galactics - 1
Forms comments
#17 opened by galactics - 1
Handle frame changing between EME2000 and GCRF
#11 opened by galactics - 0
Multiple TLE parser
#18 opened by galactics - 0
Complete SGP4/SDP4 propagator
#4 opened by galactics - 0
Predictive ordering of Node2 graphs
#2 opened by galactics - 0
- 0
Date object inner value should be in TAI
#13 opened by galactics - 0
Ephemeris object
#3 opened by galactics - 0
- 1
CIO based frames transformations
#1 opened by galactics - 0
Python classifiers
#8 opened by galactics