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	USA-80 was launched at 03:20:00 UTC on 10 April 1992, atop a ] carrier rocket, flight number D208, flying in the 7925-9.5 configuration.<ref name="LL">{{cite web\|url=http://planet4589.org/space/log/launchlog.txt\|title=Launch Log\|publisher=Jonathan's Space Page\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> The launch took place from ] at the ],<ref name="lvdb">{{cite web\|url=http://planet4589.org/space/lvdb/list2.html\|title=Launch List\|publisher=Jonathan's Space Page\|work=Launch Vehicle Database\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> and placed USA-80 into a transfer orbit. The satellite raised itself into ] using a ] ].<ref name="GSP">{{cite web\|url=http://space.skyrocket.de/doc_sdat/navstar-2a.htm\|title=GPS-2A (Navstar-2A)\|first=Gunter\|last=Krebs\|work=Gunter's Space Page\|accessdate=10 July 2012}}</ref>		USA-80 was launched at 03:20:00 UTC on 10 April 1992, atop a ] carrier rocket, flight number D208, flying in the 7925-9.5 configuration.<ref name="LL">{{cite web\|url=http://planet4589.org/space/log/launchlog.txt\|title=Launch Log\|publisher=Jonathan's Space Page\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> The launch took place from ] at the ],<ref name="lvdb">{{cite web\|url=http://planet4589.org/space/lvdb/list2.html\|title=Launch List\|publisher=Jonathan's Space Page\|work=Launch Vehicle Database\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> and placed USA-80 into a transfer orbit. The satellite raised itself into ] using a ] ].<ref name="GSP">{{cite web\|url=http://space.skyrocket.de/doc_sdat/navstar-2a.htm\|title=GPS-2A (Navstar-2A)\|first=Gunter\|last=Krebs\|work=Gunter's Space Page\|accessdate=10 July 2012}}</ref>

	On 12 May 1992, USA-80 was in an orbit with a ] of {{convert\|19979\|km}}, an ] of {{convert\|20384\|km}}, a ] of 717.94 minutes, and 55.1 degrees of ] to the equator.<ref name="satcat">{{cite web\|url=http://planet4589.org/space/log/satcat.txt\|title=Satellite Catalog\|publisher=Jonathan's Space Page\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> It had PRN 28, and operated in slot 2 of plane C of the GPS constellation. The satellite had a mass of {{convert\|1816\|kg}}. It had a design life of 7.5 years,<ref name="GSP"/> however it was retired early, on 15 August 1997. It was replaced by ].		On 12 May 1992, USA-80 was in an orbit with a ] of {{convert\|19979\|km}}, an ] of {{convert\|20384\|km}}, a ] of 717.94 minutes, and 55.1 degrees of ] to the equator.<ref name="satcat">{{cite web\|url=http://planet4589.org/space/log/satcat.txt\|title=Satellite Catalog\|publisher=Jonathan's Space Page\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> It had PRN 28, and operated in slot 2 of plane C of the GPS constellation. The satellite had a mass of {{convert\|1816\|kg}}. It had a design life of 7.5 years;<ref name="GSP"/> however, it was retired early, on 15 August 1997. It was replaced by ].

	==References==		==References==

Revision as of 02:24, 15 July 2015

USA-80
Spacecraft properties

Mission type	Navigation
Operator	US Air Force
COSPAR ID	1992-019A
SATCAT no.	21930
Mission duration	7.5 years (planned)


Spacecraft type	GPS Block IIA
Manufacturer	Rockwell
Launch mass	1,816 kilograms (4,004 lb)


Start of mission
Launch date	10 April 1992, 03:20:00 (1992-04-10UTC03:20Z) UTC
Rocket	Delta II 7925-9.5, D208
Launch site	Cape Canaveral LC-17B


End of mission
Deactivated	15 August 1997 (1997-08-16)


Orbital parameters
Reference system	Geocentric
Regime	Medium Earth (Semi-synchronous)
Perigee altitude	19,979 kilometres (12,414 mi)
Apogee altitude	20,384 kilometres (12,666 mi)
Inclination	55.1 degrees
Period	717.94 minutes

USA-80, also known as GPS IIA-4, GPS II-13 and GPS SVN-28, was an American navigation satellite which formed part of the Global Positioning System. It was the fourth of nineteen Block IIA GPS satellites to be launched.

USA-80 was launched at 03:20:00 UTC on 10 April 1992, atop a Delta II carrier rocket, flight number D208, flying in the 7925-9.5 configuration. The launch took place from Launch Complex 17B at the Cape Canaveral Air Force Station, and placed USA-80 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-37XFP apogee motor.

On 12 May 1992, USA-80 was in an orbit with a perigee of 19,979 kilometres (12,414 mi), an apogee of 20,384 kilometres (12,666 mi), a period of 717.94 minutes, and 55.1 degrees of inclination to the equator. It had PRN 28, and operated in slot 2 of plane C of the GPS constellation. The satellite had a mass of 1,816 kilograms (4,004 lb). It had a design life of 7.5 years; however, it was retired early, on 15 August 1997. It was replaced by USA-117.

References

^ "Navstar 2A-04". US National Space Science Data Center. Retrieved 10 July 2012.
^ Krebs, Gunter. "GPS-2A (Navstar-2A)". Gunter's Space Page. Retrieved 10 July 2012.
^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 10 July 2012.
^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 10 July 2012.
McDowell, Jonathan. "Launch List". Launch Vehicle Database. Jonathan's Space Page. Retrieved 10 July 2012.

v t e NAVSTAR Global Positioning System satellites
List of GPS satellites
Block I	1 2 3 4 5 6 7† 8 9 10 11
Block II	1 2 3 4 5 6 7 8 9
Block IIA	1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19
Block IIR	1† 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21
Block IIRM	1 2 3 4 5 6 7 8
Block IIF	1 2 3 4 5 6 7 8 9 10 11 12
Block III	01 02 03 04 05 06 07 08 09 10
Block IIIF	11 12 13 14 15 16 17 18 19 20
Italics indicate future missions. Signs † indicate launch failures.

v t e ← 1991 Orbital launches in 1992 1993 →
January	Kosmos 2175 STS-42 Kosmos 2176 Progress M-11 Kosmos 2177, Kosmos 2178, Kosmos 2179
February	Unnamed USA-78 Fuyo 1 Kosmos 2180 USA-79 Superbird B1, Arabsat 1C
March	Molniya 1-83 Kosmos 2181 Galaxy 5 Soyuz TM-14 STS-45
April	Kosmos 2182 Gorizont No.36L Kosmos 2183 USA-80 Kosmos 2184 Telecom 2B, Inmarsat-2 F4 Progress M-12 USA-81 Resurs-F2 No.8 Kosmos 2185
May	STS-49 Palapa B4 SROSS-C Kosmos 2186
June	Kosmos 2187, Kosmos 2188, Kosmos 2189, Kosmos 2190, Kosmos 2191, Kosmos 2192, Kosmos 2193, Kosmos 2194 EUVE Intelsat K Resurs-F1 No.55 STS-50 Progress M-13
July	Kosmos 2195 USA-82 SAMPEX USA-83 Kosmos 2196 INSAT-2A, Eutelsat-2 F4 Kosmos 2197, Kosmos 2198, Kosmos 2199, Kosmos 2200, Kosmos 2201, Kosmos 2202 Gorizont No.37L Geotail, DUVE Kosmos 2203 Soyuz TM-15 Kosmos 2204, Kosmos 2205, Kosmos 2206 Kosmos 2207 STS-46 (EURECA, TSS-1)
August	Molniya 1-84 FSW-13 TOPEX/Poseidon, Uribyol 1, S80/T Kosmos 2208 Optus B1 Progress M-14 Resurs-F1 No.54, Pion-Germes 1, Pion-Germes 2 Galaxy 1R Satcom C4
September	USA-84 Kosmos 2209 Hispasat 1A, Satcom C3 STS-47 Kosmos 2210 Mars Observer
October	FSW-14, Freja Foton No.8L DFS-Kopernikus 3 Molniya-3 No.50 Kosmos 2211, Kosmos 2212, Kosmos 2213, Kosmos 2214, Kosmos 2215, Kosmos 2216 Kosmos 2217 STS-52 (LAGEOS-2, CTA) Progress M-15 (Znamya-2) Galaxy 7 Kosmos 2218 Ekran-M No.15L
November	Resurs 500 Kosmos 2219 Kosmos 2220 MSTI-1 USA-85 Kosmos 2221 Kosmos 2222 Gorizont No.38L USA-86
December	Superbird A1 Molniya-3 No.56 STS-53 (USA-89, ODERACS) Kosmos 2223 Kosmos 2224 USA-87 Optus B2 Kosmos 2226 Kosmos 2225 Kosmos 2227 Kosmos 2228 Kosmos 2229
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).

This article about one or more spacecraft of the United States is a stub. You can help Misplaced Pages by expanding it.

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Revision as of 00:32, 18 January 2015 editFiledelinkerbot (talk \| contribs)Bots, Rollbackers275,832 edits Bot: Removing Commons:File:Navstar-2.jpg (en). It was deleted on Commons by Green Giant (Per Commons:Commons:Deletion requests/File:Navstar-2.jpg).← Previous edit		Revision as of 02:24, 15 July 2015 edit undoWavelength (talk \| contribs)Extended confirmed users, Pending changes reviewers179,502 edits MOS:HOWEVERPUNC—Radio announcers, please pause. Radio listeners, please wait. Please do not confuse the adverb "however" with the conjunction "but".Next edit →
Line 45:		Line 45:
	USA-80 was launched at 03:20:00 UTC on 10 April 1992, atop a ] carrier rocket, flight number D208, flying in the 7925-9.5 configuration.<ref name="LL">{{cite web\|url=http://planet4589.org/space/log/launchlog.txt\|title=Launch Log\|publisher=Jonathan's Space Page\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> The launch took place from ] at the ],<ref name="lvdb">{{cite web\|url=http://planet4589.org/space/lvdb/list2.html\|title=Launch List\|publisher=Jonathan's Space Page\|work=Launch Vehicle Database\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> and placed USA-80 into a transfer orbit. The satellite raised itself into ] using a ] ].<ref name="GSP">{{cite web\|url=http://space.skyrocket.de/doc_sdat/navstar-2a.htm\|title=GPS-2A (Navstar-2A)\|first=Gunter\|last=Krebs\|work=Gunter's Space Page\|accessdate=10 July 2012}}</ref>		USA-80 was launched at 03:20:00 UTC on 10 April 1992, atop a ] carrier rocket, flight number D208, flying in the 7925-9.5 configuration.<ref name="LL">{{cite web\|url=http://planet4589.org/space/log/launchlog.txt\|title=Launch Log\|publisher=Jonathan's Space Page\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> The launch took place from ] at the ],<ref name="lvdb">{{cite web\|url=http://planet4589.org/space/lvdb/list2.html\|title=Launch List\|publisher=Jonathan's Space Page\|work=Launch Vehicle Database\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> and placed USA-80 into a transfer orbit. The satellite raised itself into ] using a ] ].<ref name="GSP">{{cite web\|url=http://space.skyrocket.de/doc_sdat/navstar-2a.htm\|title=GPS-2A (Navstar-2A)\|first=Gunter\|last=Krebs\|work=Gunter's Space Page\|accessdate=10 July 2012}}</ref>

	On 12 May 1992, USA-80 was in an orbit with a ] of {{convert\|19979\|km}}, an ] of {{convert\|20384\|km}}, a ] of 717.94 minutes, and 55.1 degrees of ] to the equator.<ref name="satcat">{{cite web\|url=http://planet4589.org/space/log/satcat.txt\|title=Satellite Catalog\|publisher=Jonathan's Space Page\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> It had PRN 28, and operated in slot 2 of plane C of the GPS constellation. The satellite had a mass of {{convert\|1816\|kg}}. It had a design life of 7.5 years,<ref name="GSP"/> however it was retired early, on 15 August 1997. It was replaced by ].		On 12 May 1992, USA-80 was in an orbit with a ] of {{convert\|19979\|km}}, an ] of {{convert\|20384\|km}}, a ] of 717.94 minutes, and 55.1 degrees of ] to the equator.<ref name="satcat">{{cite web\|url=http://planet4589.org/space/log/satcat.txt\|title=Satellite Catalog\|publisher=Jonathan's Space Page\|first=Jonathan\|last=McDowell\|accessdate=10 July 2012}}</ref> It had PRN 28, and operated in slot 2 of plane C of the GPS constellation. The satellite had a mass of {{convert\|1816\|kg}}. It had a design life of 7.5 years;<ref name="GSP"/> however, it was retired early, on 15 August 1997. It was replaced by ].

	==References==		==References==