NSS-5

{{Use American English|date=February 2014}}

{{Use mdy dates|date=February 2014}}

{{Infobox spaceflight

| name = Intelsat 803 → NSS-5

| image =

| image_caption =

| mission_type = Communications

| operator = IntelsatSES World Skies

| website =

| COSPAR_ID = 1997-053A

| SATCAT = 24957

| mission_duration = 14 years

| spacecraft_bus =

| spacecraft_type = AS-7000

| manufacturer = Lockheed Martin

| dry_mass =

| BOL_mass =

| launch_mass = {{convert|3412|kg|lb}}

| dimensions =

| power =

| launch_date = {{start-date|September 23, 1997, 23:58|timezone=yes}} UTC{{cite web|url=http://planet4589.org/space/log/launchlog.txt|title=Launch Log|first=Jonathan|last=McDowell|work=Jonathan's Space Page|access-date=May 5, 2017}}

| launch_rocket = Ariane-42L H10-3

| launch_site = Kourou ELA-2

| launch_contractor = Arianespace

| disposal_type =

| deactivated =

| orbit_epoch = May 5, 2017{{cite web|url=http://www.n2yo.com/satellite/?s=24957|title=NSS 5 (INTELSAT 803 )|work=N2YO|access-date=May 5, 2017}}

| orbit_reference = Geocentric

| orbit_regime = Geostationary

| orbit_periapsis = {{convert|35,778.2|km|mi}}

| orbit_apoapsis = {{convert|35,809.1|km|mi}}

| orbit_inclination = 3.8 degrees

| orbit_semimajor = {{convert|42,164.0|km|mi}}

| orbit_period = 1,436.1 minutes

| orbit_longitude = 50.5° E

| apsis = gee

| trans_band = 38 C Band, 6 Ku band

| trans_frequency =

| trans_bandwidth =

| trans_capacity =

| trans_coverage = Pacific Ocean

| trans_TWTA =

| trans_EIRP =

| trans_HPBW =

| programme = Intelsat 8

| previous_mission = Intelsat 802

| next_mission = Intelsat 804

}}

NSS-5 (Formerly known as Intelsat 803 and NSS-803) is a communications satellite operated by Intelsat and after by SES World Skies. Launched in 1997 it was operated in geostationary orbit at a longitude of 50.5 degrees east for around 14 years.

Satellite

The third of six Intelsat VIII satellites to be launched, NSS-5 was built by Lockheed Martin. It was a {{convert|3412|kg|lb|adj=on}} spacecraft. The satellite carried a double LEROS-1B apogee motor for propulsion and was equipped with 38 C Band transponders and 6 Ku band transponders, powered by 2 solar cells more batteries. It was designed for a fourteen-year service life.{{cite web|url=http://space.skyrocket.de/doc_sdat/intelsat-8.htm|title=Intelsat-8 (801, 802, 803, 804) / NSS 803 → NSS 5|first=Gunter|last=Krebs|work=Gunter's Space Page|access-date=May 5, 2017}}

Launch

The launch of NSS-5 made use of an Ariane 4 rocket flying from Guiana Space Centre, Kourou, French Guiana. The launch took place at 23:58 UTC on September 23, 1997, with the spacecraft entering a geosynchronous transfer orbit. NSS-5 subsequently fired its apogee motor to achieve geostationary orbit.

See also

{{Portal|Spaceflight}}

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References

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{{Intelsat}}

{{SES satellites}}

{{Orbital launches in 1997}}

Category:Intelsat satellites

Category:SES satellites

Category:Spacecraft launched in 1997

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