Bjorn, > If the orbit is circular at 213 km after the first burn, how can Breez be > at 1739 km at the 2nd burn ? > End of burn given? If so, why not also give time and position of the > start of each burn ? Briz-M (Breeze-M) engine is relatively low-thrust (2000 kgf if memory serves) and each burn is long. > Elements for the previous Breez launches are available at > http://hea-www.harvard.edu/QEDT/jcm/space/elements/26700/S26738 > http://hea-www.harvard.edu/QEDT/jcm/space/elements/26700/S26737 > http://hea-www.harvard.edu/QEDT/jcm/space/elements/26700/S26736 > http://hea-www.harvard.edu/QEDT/jcm/space/elements/26300/S26377 > http://hea-www.harvard.edu/QEDT/jcm/space/elements/26300/S26373 > http://hea-www.harvard.edu/QEDT/jcm/space/elements/26300/S26372 > but the elsets start with MM=2.32 or lower. > > There is no time to request other (?) elsets from OIG. Anyone have > earlier elsets? For both launches, I have all elsets from OIG but none with MM < 2.3. Igor Lissov ----------------------------------------------------------------- Unsubscribe from SeeSat-L by sending a message with 'unsubscribe' in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org http://www.satellite.eu.org/seesat/seesatindex.html
This archive was generated by hypermail 2b29 : Sun Dec 29 2002 - 08:03:49 EST