OEMEphemeris
Ephemeris data in Orbit Ephemeris Message (OEM) format.
Position, velocity, and acceleration units must be represented in km, km/s, and
km/s^2, respectively, in ephemeris data lines. Covariance matrix line units must be
represented in km^2 if computed from two positions, km^2/s if computed from one
position and one velocity, and km^2/s^2 if computed from two velocities. Consult section
7.7.2 of The Consultative Committee for Space Data Systems (CCSDS)
Recommended Standard for Orbit Data Messages
Contents
- oemData
-
The data for an OEM ephemeris, supplied directly in the request rather than through an S3 object.
Type: String
Length Constraints: Minimum length of 1.
Pattern:
^[\s\S]+$Required: No
- s3Object
-
Identifies the S3 object to be used as the ephemeris.
Type: S3Object object
Required: No
See Also
For more information about using this API in one of the language-specific AWS SDKs, see the following:
