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CelestLab >> Orbit properties > CL_op_frozenOrbit

CL_op_frozenOrbit

Eccentricity and argument of periapsis of a frozen orbit

Calling Sequence

[ecc,pom] = CL_op_frozenOrbit(sma,inc,[,er,zonals])

Description

Parameters

sma:

Semi major axis [m] (1xN or 1x1)

inc:

Inclination [rad] (1xN or 1x1)

er:

(optional) Equatorial radius [m]. Default is %CL_eqRad.

zonals:

(optional) Vector of zonal coefficients J1 to Jn (1xNz or Nzx1). Default is %CL_j1jn(1:3).

ecc:

Mean eccentricity (1xN)

pom:

Mean argument of periapsis [rad] (1xN)

Authors

Examples

sma = %CL_eqRad + [350.e3, 700.e3];
inc = CL_deg2rad(98);
[ecc,pom] = CL_op_frozenOrbit(sma,inc)
[ecc,pom] = CL_op_frozenOrbit(sma,inc,zonals=%CL_j1jn(1:20))
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