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NATO 3A, 8808

Orbit data source: Space-Track

NATO 3A, 8808 is a payload satellite owned by NICSMA (NATO) in GEO that was launched on Thu, 22 Apr 1976 UTC via a DELTA 2914 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Iframe URL

https://www.satcat.com/sats-embedded/8808?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

8808, 1976-035A

Orbit

GEO

Country

Unknown / NATO

Related business

North Atlantic Treaty Organization (NATO) (BE)

Manufacturer

Ae Ford WDL

Mission

Spacecraft

Bus & Motor

NATO 3, SVM-6

Mass

670 kg wet, 249 kg dry

Launch date (UTC)

1976-04-22 (50 years ago)

Launch vehicle

DELTA 2914

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

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Last TLE update: 16 hours ago

TLE from 16 hours ago

0 NATO 3A
1 08808U 76035A   26054.29412625 -.00000059  00000-0  00000-0 0  9998
2 08808   5.2352 298.7242 0027202 327.6404 253.0382  0.99836562746138

Epoch: 2026-02-23T07:03Z

TLE epoch observation values (Epoch: 2026-02-23T07:03:32.508Z)

Latitude

-3.3834°

Longitude

-100.05603°

Altitude

35,943.051 km

Speed

3.068 km/s

True Right ascension

10h 36m 04s

True Declination

-3° 22' 48"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

02:25:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

36,025.134 km

Perigee altitude

35,795.069 km

Semi-major axis

42,288.238 km

Eccentricity

0.00272

Inclination

5.2352°

RAAN

298.7242°

Arg. of periapsis

327.6404°

True anomaly

252.74034°

Mean anomaly

253.0382°

Eccentric anomaly

252.88924°

Mean motion

0.24958 °/min

Orbital period

1,442.41 mins

BSTAR

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Other satellites on launch #35 in the year 1976 (1976-04-22 UTC)

DELTA 1 R/B(2), 8810 (Decayed)

DELTA 1 R/B(1), 8809 (Decayed)

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NATO 3A Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
1440 mins	2026-02-23 23:10:55.638Z	171.84° S	2026-02-24 22:27:55.638Z	174.462° S	37.288°	2026-02-24 23:10:55.638Z	174.545° S

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8808 neighbors

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out NATO 3A, 8808 on other resources

View NATO 3A, 8808 on NASA - NSSDCA Website

View NATO 3A, 8808 on Heavens-Above

View NATO 3A, 8808 on Keep Track

View NATO 3A, 8808 on Celestrak

View NATO 3A, 8808 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

NATO 3A, 8808

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-02-23T07:03:32.508Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #35 in the year 1976 (1976-04-22 UTC)

NATO 3A Visibility forecast

8808 neighbors

Co-orbital & Co-planar RSOs

Check out NATO 3A, 8808 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago