ERS-1 Mission Phase E


Phase E parameters

Phase E parameters

Orbit number characteristics

Orbit parameters


Formulas from Relative (track) to Absolute Orbit Number

ABS_ORB_NUM = REL_ORB_NUM + (CYCLE_NUM-139)*2411 +12510

CYCLE_NUM = INT( ( ABS_ORB_NUM-12511)/2411 ) + 139

REL_ORB_NUM= ABS_ORB_NUM -12510 -(CYCLE_NUM-139) *2411

Where:


GDS This information was retrieved from ESA/ESRIN
DEOS Home This page is maintained by
Remko Scharroo, remko.scharroo@lr.tudelft.nl