DEIMOS
Earth Observation Mission CFI Software
Orbit Software User Manual
for JAVA
ESA

EECFI.OrbitalInfo Class Reference

Orbital information. More...

List of all members.

Public Member Functions

 OrbitalInfo ()
 Empty constructor.
 OrbitalInfo (long absOrb, long repCyc, long cycLen, double mlstDriftIn, double mlstIn, double anxLon, double utc, double[] pos, double[] vel, double[] meanKepl, double[] oscKepl, double nodPeriod, double utcSMX)
 Constructor with parameters.

Public Attributes

long absOrbit
 Absolute orbit.
long repCycle
 Repeat cycle.
long cycLength
 Cycle length.
double mlstDrift
 MLST drift (seconds/day).
double mlst
 Mean Local Solar Time (hours).
double phasing
 Longitude at ascending node (deg).
double utcAnx
 UTC time at ascending node (days, processing format).
double[] posAnx
 Position at ascending node (m).
double[] velAnx
 Velocity at Ascending node (m/s).
double[] meanKep
 Mean keplerian elements.
double[] oscKep
 Osculating keplerian elements.
double nodalPeriod
 Nodal period of orbit (s).
double utcSmx
 UTC time at Spacecraft Midnight [days, processing format].

Detailed Description

Orbital information.


Constructor & Destructor Documentation

EECFI.OrbitalInfo.OrbitalInfo (  ) 

Empty constructor.

EECFI.OrbitalInfo.OrbitalInfo ( long  absOrb,
long  repCyc,
long  cycLen,
double  mlstDriftIn,
double  mlstIn,
double  anxLon,
double  utc,
double[]  pos,
double[]  vel,
double[]  meanKepl,
double[]  oscKepl,
double  nodPeriod,
double  utcSMX 
)

Constructor with parameters.


Member Data Documentation

Absolute orbit.

Cycle length.

Mean keplerian elements.

Mean Local Solar Time (hours).

MLST drift (seconds/day).

Nodal period of orbit (s).

Osculating keplerian elements.

Longitude at ascending node (deg).

Position at ascending node (m).

Repeat cycle.

UTC time at ascending node (days, processing format).

UTC time at Spacecraft Midnight [days, processing format].

Velocity at Ascending node (m/s).


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