PAGEOS

Passive geodetic satellite launched by NASA in 1966


title: "PAGEOS" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["geodetic-satellites", "satellites-formerly-orbiting-earth", "passive-satellites", "spacecraft-launched-in-1966", "balloon-satellites"] description: "Passive geodetic satellite launched by NASA in 1966" topic_path: "general/geodetic-satellites" source: "https://en.wikipedia.org/wiki/PAGEOS" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary Passive geodetic satellite launched by NASA in 1966 ::

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

FieldValue
namePassive Geodetic Earth Orbiting Satellite (PAGEOS)
names_listPAGEOS-A
image
image_captionTest inflation of PAGEOS, 5 August 1965
image_alt
image_size
mission_type
operatorNASA Office of Space Applications
COSPAR_ID1966-056A
SATCAT02253
website
mission_duration
distance_travelled
orbits_completed
suborbital_range
suborbital_apogee
spacecraft
spacecraft_type
spacecraft_bus
manufacturer
launch_mass56.7 kg
BOL_mass
landing_mass
dry_mass
payload_mass
dimensions30.48 m diameter
power
launch_date
launch_rocketThrust augmented Thor-Agena D
launch_siteVandenberg AFB
launch_contractor
deployment_from
deployment_date
entered_service
disposal_type
deactivated
destroyedpartially disintegrated
last_contact
recovery_by
recovery_date
decay_date
landing_date
landing_site
{{end dateYYYY
orbit_reference
orbit_regime
orbit_longitude
orbit_slot
orbit_semimajor
orbit_eccentricity0.00301
orbit_periapsis4207 km
orbit_apoapsis4271 km
orbit_inclination87.14°
orbit_period181.43 min
orbit_RAAN
orbit_arg_periapsis
orbit_mean_anomaly
orbit_mean_motion
orbit_repeat
orbit_velocity
orbit_epoch24 June 1966
orbit_rev_number
apsisgee
next_mission
insignia
insignia_caption
insignia_alt
insignia_size
::

| name = Passive Geodetic Earth Orbiting Satellite (PAGEOS) | names_list = PAGEOS-A

| image = Image:PAGEOS Satellite - GPN-2000-001896.jpg | image_caption = Test inflation of PAGEOS, 5 August 1965 | image_alt = | image_size = | mission_type = | operator = NASA Office of Space Applications | Harvard_designation = | COSPAR_ID = 1966-056A | SATCAT = 02253 | website = | mission_duration = | distance_travelled = | orbits_completed = | suborbital_range = | suborbital_apogee =

| spacecraft = | spacecraft_type = | spacecraft_bus = | manufacturer = | launch_mass = 56.7 kg | BOL_mass = | landing_mass = | dry_mass = | payload_mass = | dimensions = 30.48 m diameter | power =

| launch_date = | launch_rocket = Thrust augmented Thor-Agena D | launch_site = Vandenberg AFB | launch_contractor = | deployment_from = | deployment_date = | entered_service =

| disposal_type = | deactivated = | destroyed = partially disintegrated | last_contact = | recovery_by = | recovery_date = | decay_date = | landing_date = | landing_site = The following template should be used for ONE of the three above fields "end_of_mission", "decay" or "landing" if the spacecraft is no longer operational. If it landed intact, use it for the landing time, otherwise for the date it ceased operations, or the decay date if it was still operational when it re-entered. (for Zulu/UTC) or (if time unknown)

| orbit_reference = Geocentric | orbit_regime = | orbit_longitude = | orbit_slot = | orbit_semimajor = | orbit_eccentricity = 0.00301 | orbit_periapsis = 4207 km | orbit_apoapsis = 4271 km | orbit_inclination = 87.14° | orbit_period = 181.43 min | orbit_RAAN = | orbit_arg_periapsis = | orbit_mean_anomaly = | orbit_mean_motion = | orbit_repeat = | orbit_velocity = | orbit_epoch = 24 June 1966 | orbit_rev_number = | apsis = gee

If in doubt, leave it out--| programme = | previous_mission = | next_mission = | insignia = | insignia_caption = | insignia_alt = | insignia_size =

PAGEOS (PAssive Geodetic Earth Orbiting Satellite) was a balloon satellite which was launched by NASA in June 1966. It was the first satellite specifically launched for use in geodetic surveying, or measuring the shape of the earth, by serving as a reflective and photographic tracking target. At the time, it improved on terrestrial triangulations of the globe by about an order of magnitude. The satellite, which carried no instrumentation, broke up between 1975 and 1976. One of the largest fragments of the satellite finally deorbited in 2016.

PAGEOS was part of a larger program of inflatable satellites that grew from the original concept by William J. O'Sullivan of a 30-inch diameter inflatable satellite in 1956 to measure air drag at high altitudes, called the Sub-Satellite. While the Sub-Satellite failed, the idea of a visible US satellite became very attractive after Sputnik launched in the Cold War, resulting in a program of similar, larger satellites. These included satellites Echo 1 and Echo 2 under Project Echo, which were also used for experiments in geodetic surveying; several air-density-focused Explorer satellites; and finally PAGEOS.

Design

PAGEOS had a diameter of exactly 100 ft, consisted of a 0.5 mil thick mylar plastic film coated with vapour deposited aluminum enclosing a volume of about 524000 cuft The metal coating both reflected sunlight and protected the satellite from damaging ultraviolet waves. The satellite was launched in a canister, which explosively separated as it was ejected from the rocket. Then, the balloon was inflated through a combination of residual internal air and a mixture of benzoic acid and anthraquinone placed inside, which turned to gas when the satellite was exposed to the heat of the sun. The satellite carried no instrumentation. The study and construction of PAGEOS was done by the Schjeldahl company, which also made Echo 1.

Usage

::figure[src="https://upload.wikimedia.org/wikipedia/commons/c/c7/BC-4_World_Primary_Network.jpg" caption="Network of BC4 cameras used to establish the Worldwide Geometric Satellite Triangulation Network"] ::

::figure[src="https://upload.wikimedia.org/wikipedia/commons/e/ed/BC4_camera_inside_observing_dome.jpg" caption="section"] ::

| date = January 2025 | reason = Different sources on the topic appear to contradict each other PAGEOS was placed into a polar orbit, about 200 nautical miles above the earth, so that the U.S. Coastal and Geodetic Survey could practically apply triangulation techniques developed from experiments with Echo 1. This program was known as the "Worldwide Geometric Satellite Triangulation Program". Because of the satellite's high altitude, the sun illuminated it during the entirety of Earth night, allowing it to be picked out from a background of stars. Over five years, 16 groups conducted observations at 45 globally distributed stations, about 3000-4000 km apart from each other. 12 mobile tracking stations were used, which observed during favorable weather conditions during a few minutes of twilight each evening. BC4 cameras were used to photograph the satellite. Observations were taken when the satellite was visible simultaneously to multiple stations at the same time. This resulted in the fixing of the precise locations of 38 different points around the world. This could be used to help determine the precise locations of the continents relative to each other, and to help determine the precise shape and size of the earth. Some unclassified data was used by scientists studying continental drift, and more classified data was used by US military planners studying intercontinental ballistic missiles. The observations were done with BC4 (Ballistic Camera-4) cameras, and could last more than a year at each station before satisfactory results were obtained. The network reached an accuracy about an order of magnitude better than terrestrial triangulations at the time, and was the first time that a scientific determination had been made with accuracy of a complete global polyhedron.

Orbit

::figure[src="https://upload.wikimedia.org/wikipedia/commons/3/34/Thor-SLV2A_Agena-D_(Thor_473)_with_PAGEOS.jpg" caption="Thor-SLV2A Agena-D launching PAGEOS"] ::

The PAGEOS spacecraft was launched by a Thor-SLV2A Agena-D (Thor 473) on 24 June 1966, and placed into a polar orbit (inclination 85–86°) with an initial height of 4200km, which had gradually lowered during its 9 years of operation. The satellite first partly disintegrated in July 1975, which was followed by a second break-up that occurred in January 1976 resulting in the release of a large number of fragments. Most of these re-entered during the following decade. In 2016, one of the largest fragments of PAGEOS de-orbited.

The satellite's orbital period was approximately three hours. It was about as bright as Polaris, and appeared as a slow-moving star. Thanks to its high orbit and its polar inclination, it did not pass through the Earth's shadow and was visible any time of night, unlike lower-orbit satellites which had to be viewed exclusively just before sunrise and after sunset. Its high orbit also allowed it to be seen simultaneously by observers 2000-3000 km apart at optimum distances from the zenith.

References

References

  1. "NSSDCA – PAGEOS 1 – Trajectory Details". [[NASA]].
  2. "PAGEOS 1".
  3. "Modern Surveying".
  4. Kleusberg, Alfred. (2003). "Satelliten im Dienst der Geodäsie und Geoinformatik".
  5. Hansen, James. (12 March 2013). "Spaceflight Revolution: NASA Langley Research Center from Sputnik to Apollo". Cia Publishing.
  6. Teichman, L. A. (June 1, 1968). [https://ntrs.nasa.gov/citations/19680016348 "The fabrication and testing of Pageos 1"]. ''NASA Technical Reports Server''
  7. (19 June 1966). "Pageos Satellite to Girdle Globe for Earth Mapping".
  8. (2007). "Entering the Space Age: The Evolution of Satellite Geodesy at the Coast and Geodetic Survey". National Oceanic and Atmospheric Administration.
  9. Seeber, Günter. (2008-08-22). "Satellite Geodesy: Foundations, Methods, and Applications". Walter de Gruyter.
  10. Krebs, Gunter D. "Thor-SLV2A Agena-D".
  11. Henriksen, S. W.. (1 January 1977). "National Geodetic Satellite Program, Part 1".
  12. Krebs, Gunter D. "PAGEOS 1".
  13. J.-C. Liou. (February 1, 2017). "USA Space Debris Environment, Operations, and Research Updates". 54th Session of the Scientific and Technical Subcommittee, Committee on the Peaceful Uses of Outer Space, United Nations, 30 January – 10 February 2017, Vienna.
  14. Dicati, Renato. (2017-01-10). "Stamping the Earth from Space". Springer.

::callout[type=info title="Wikipedia Source"] This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page. ::

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