diff --git a/clients/client-groundstation/src/models/models_0.ts b/clients/client-groundstation/src/models/models_0.ts index aeed48fd0938..4e0871d4ff52 100644 --- a/clients/client-groundstation/src/models/models_0.ts +++ b/clients/client-groundstation/src/models/models_0.ts @@ -2092,13 +2092,7 @@ export interface S3Object { * 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
- * for more information.
+ * AWS Ground Station processes OEM Customer Provided Ephemerides according to the CCSDS standard with some extra restrictions. OEM files should be in KVN format. For more detail about the OEM format that AWS Ground Station supports, see OEM ephemeris format in the AWS Ground Station user guide.
*
- * 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
- * for more information.
+ * AWS Ground Station processes OEM Customer Provided Ephemerides according to the CCSDS standard with some extra restrictions. OEM files should be in KVN format. For more detail about the OEM format that AWS Ground Station supports, see OEM ephemeris format in the AWS Ground Station user guide.
*
\n Ephemeris data in Orbit Ephemeris Message (OEM) format.\n
\n\n Position, velocity, and acceleration units must be represented in km
, km/s
, and\n km/s**2
, respectively, in ephemeris data lines. Covariance matrix line units must be\n represented in km**2
if computed from two positions, km**2/s
if computed from one\n position and one velocity, and km**2/s**2
if computed from two velocities. Consult section\n 7.7.2 of The Consultative Committee for Space Data Systems (CCSDS)\n Recommended Standard for Orbit Data Messages\n for more information.\n
\n Ephemeris data in Orbit Ephemeris Message (OEM) format.\n
\n\n AWS Ground Station processes OEM Customer Provided Ephemerides according to the CCSDS standard with some extra restrictions. OEM files should be in KVN format. For more detail about the OEM format that AWS Ground Station supports, see OEM ephemeris format in the AWS Ground Station user guide.\n
" } }, "com.amazonaws.groundstation#PaginationMaxResults": {