OPS 9794

American navigation satellite used for GPS


title: "OPS 9794" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["spacecraft-launched-in-1981", "gps-satellites", "satellite-launch-failures", "1983-in-spaceflight"] description: "American navigation satellite used for GPS" topic_path: "general/spacecraft-launched-in-1981" source: "https://en.wikipedia.org/wiki/OPS_9794" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary American navigation satellite used for GPS ::

::data[format=table title="Infobox spaceflight"]

FieldValue
nameOPS 9794
names_listNavstar 8
GPS I-8
GPS SVN-8
image_size290px
mission_typeNavigation
Technology
operatorU.S. Air Force
COSPAR_ID1983-072A
SATCAT14189
mission_duration5 years (planned)
9.75 years (achieved)
spacecraftNavstar
spacecraft_typeGPS Block I
manufacturerRockwell Space Systems
launch_mass758 kg
dimensions5.3 meters long
power400 watts
launch_date14 July 1983, 10:21:00 UTC
launch_rocketAtlas E / SGS-2
(Atlas-75E)
launch_siteVandenberg, SLC-3W
entered_service10 August 1983
deactivated4 May 1993
orbit_referenceGeocentric orbit
orbit_regimeMedium Earth orbit
(Semi-synchronous)
orbit_periapsis19917 km
orbit_apoapsis20446 km
orbit_inclination62.80°
orbit_period718.00 minutes
apsisgee
programmeGlobal Positioning System
previous_missionNavstar 7
next_missionUSA-1 (Navstar 9)
::

| name = OPS 9794 | names_list = Navstar 8 GPS I-8 GPS SVN-8 | image = | image_caption = | image_size = 290px

| mission_type = Navigation Technology | operator = U.S. Air Force | COSPAR_ID = 1983-072A | SATCAT = 14189 | mission_duration = 5 years (planned) 9.75 years (achieved)

| spacecraft = Navstar | spacecraft_type = GPS Block I | manufacturer = Rockwell Space Systems | launch_mass = 758 kg | dimensions = 5.3 meters long | power = 400 watts

| launch_date = 14 July 1983, 10:21:00 UTC | launch_rocket = Atlas E / SGS-2 (Atlas-75E) | launch_site = Vandenberg, SLC-3W

| entered_service = 10 August 1983 | deactivated = 4 May 1993

| orbit_reference = Geocentric orbit | orbit_regime = Medium Earth orbit (Semi-synchronous) | orbit_slot = | orbit_periapsis = 19917 km | orbit_apoapsis = 20446 km | orbit_inclination = 62.80° | orbit_period = 718.00 minutes | apsis = gee

| programme = Global Positioning System | previous_mission = Navstar 7 | next_mission = USA-1 (Navstar 9)

OPS 9794, also known as Navstar 8, GPS I-8 and GPS SVN-8, was an American navigation satellite launched in 1983 as part of the Global Positioning System development program. It was the eighth of eleven Block I GPS satellites to be launched.

Background

Global Positioning System (GPS) was developed by the U.S. Department of Defense to provide all-weather round-the-clock navigation capabilities for military ground, sea, and air forces. Since its implementation, GPS has also become an integral asset in numerous civilian applications and industries around the globe, including recreational used (e.g., boating, aircraft, hiking), corporate vehicle fleet tracking, and surveying. GPS employs 24 spacecraft in 20,200 km circular orbits inclined at 55°. These vehicles are placed in 6 orbit planes with four operational satellites in each plane.

Spacecraft

The first eleven spacecraft (GPS Block 1) were used to demonstrate the feasibility of the GPS system. They were 3-axis stabilized, nadir pointing using reaction wheels. Dual solar arrays supplied over 400 watts. They had S-band communications for control and telemetry and Ultra high frequency (UHF) cross-link between spacecraft. They were manufactured by Rockwell Space Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block 1 spacecraft were inclined at 63°.

Launch

OPS 9794 was launched at 10:21 UTC on 14 July 1983, atop an Atlas E launch vehicle with an SGS-2 upper stage. The Atlas used had the serial number 75E, and was originally built as an Atlas E. The launch took place from Space Launch Complex 3W at Vandenberg Air Force Base, and placed OPS 9794 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-27 apogee motor.

Mission

By 10 August 1983, OPS 9794 had been raised to an orbit with a perigee of 19917 km, an apogee of 20446 km, a period of 718.00 minutes, and 62.80° of inclination to the equator. The satellite had a design life of 5 years and a mass of 758 kg. It broadcast the PRN 11 signal in the GPS demonstration constellation, and was retired from service on 4 May 1993.

References

References

  1. (14 May 2020). "Trajectory: Navstar 8 1983-072A". NASA.
  2. (14 May 2020). "Display: Navstar 8 1983-072A". NASA.
  3. McDowell, Jonathan. "Launch Log". Jonathan's Space Report.
  4. McDowell, Jonathan. "Launch List". Jonathan's Space Report.
  5. Krebs, Gunter. "GPS (Navstar)". Gunter's Space Page.
  6. McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Report.

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spacecraft-launched-in-1981gps-satellitessatellite-launch-failures1983-in-spaceflight