TECHSAT 1B
Mission information
Name
TECHSAT 1B
Alternate Names
GO-32 TechSat, Gurwin-II
Satellite ID
FCHF-0545-3706-3789-8061
NORAD ID
25397
Country of Origin

Israel

Status
Satellite alive
Operational

Satellite is in orbit and operational

Image
TECHSAT 1B
Mission timeline
Launch Date
1998-07-10T00:00:00+00:00
Description

Techsat 1b is an imaging satellite that transmits a 9600 baud burst every 30 seconds. Built by the Technion Institute of Technology in Israel it replaced Techsat 1a which failed to reach orbit.

Mode V/U APRS,BBS 9K6 FSK
Type
Transceiver
Downlink Mode
FSK
Downlink Frequency
435.225 MHz
Baud
9600
Uplink Mode
FSK
Uplink Frequency
145.930 MHz
Mode V/U APRS 9K6 FSK
Type
Transceiver
Downlink Mode
FSK
Downlink Frequency
435.225 MHz
Baud
9600
Uplink Mode
FSK
Uplink Frequency
145.850 MHz
Mode V/U BBS 9k6 FSK
Type
Transceiver
Downlink Mode
FSK
Downlink Frequency
435.225 MHz
Baud
9600
Uplink Mode
FSK
Uplink Frequency
145.890 MHz
Mode L/U 9K6 FSK
Type
Transceiver
Downlink Mode
FSK
Downlink Frequency
435.225 MHz
Baud
9600
Uplink Mode
FSK
Uplink Frequency
1269.900 MHz
Mode L/U 9K6 FSK
Type
Transceiver
Downlink Mode
FSK
Downlink Frequency
435.225 MHz
Baud
9600
Uplink Mode
FSK
Uplink Frequency
1269.800 MHz
Mode L/U 9K6 FSK
Type
Transceiver
Downlink Mode
FSK
Downlink Frequency
435.225 MHz
Baud
9600
Uplink Mode
FSK
Uplink Frequency
1269.700 MHz
Mode U 9k6 FSK
Type
Transmitter
Service
Amateur
Downlink Mode
FSK
Downlink Frequency
435.225 MHz
Baud
9600
Mode U 9k6 FSK
Type
Transmitter
Service
Amateur
Downlink Mode
FSK
Downlink Frequency
435.325 MHz
Downlink Drifted
435.324 MHz
Baud
9600
Most Recent Observers (last 24h)
Observer Latest Data
ISAE.Supaero UHF/VHF-JN03rn 2025-07-09 16:48:25 UTC
EU1AEM-KO33nv 2025-07-09 15:06:49 UTC
M0GLU-IO91vc 2025-07-09 15:05:19 UTC
PF_DE_UHF_X_DIPOLE-JN48iv 2025-07-09 15:03:44 UTC
DF0OHM Turnstile VHF (Test UHF)-JN59nk 2025-07-09 15:02:34 UTC
Data Frames Decoded - 30 Days
There is no decoded data for this satellite in the last 30 days.
No Decoders Found
Help us develop a decoder, you can find instructions at this wiki link
Orbital Elements
Latest Two-Line Element (TLE)
TLE Source
CalPoly
TLE Updated
2025-07-09 11:02:34 UTC
TLE Set
1 25397U 98043D   25189.84497884  .00000035  00000-0  35068-4 0  9991
2 25397 98.9715 169.5769 0002278 108.7415 251.4010 14.24320997402454
Satellite Suggestion History

Transmitter Suggestion History