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INTELSAT 2-F1, 2514

Orbit data source: Space-Track

INTELSAT 2-F1, 2514 is a payload satellite owned by INTELSAT (US) in HEO that was launched on Wed, 26 Oct 1966 UTC via a THOR DELTA E1 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 src="https://www.satcat.com/sats-embedded/2514?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/2514?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2514, 1966-096A

Orbit

HEO

Last TLE update

1 day ago

Origin

Intelsat (Unknown / ITSO)

Manufacturer

Hughes

Mission

Non-operational Civil Communications

Bus & Motor

HS-303, SVM-1

Mass

162 kg wet, 64 kg dry

Launch date (UTC)

1966-10-26 (59 years ago)

Launch vehicle

THOR DELTA E1

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.4 m

Radar Cross Section

2.199 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 INTELSAT 2-F1
1 02514U 66096A   25185.63931876 -.00000337  00000-0  00000-0 0  9997
2 02514  17.1632 122.0038 6351695  59.5049 347.9589  2.00537581 87840

Epoch: 2025-07-04T15:20Z

TLE epoch observation values (Epoch: 2025-07-04T15:20:37.14Z)

Latitude

0.00017°

Longitude

-31.15129°

Altitude

5,634.581 km

Speed

7.166 km/s

True Right ascension

08h 07m 34s

True Declination

0° 00' 01"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-15.81889°

Longitude

-144.86461°

Altitude

36,409.523 km

Speed

1.904 km/s

Apparent Right ascension

00h 19m 47s

Apparent Declination

-19° 05' 46"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

10:26:37

Azimuth

302.293° NW

Elevation

-58.01°

Doppler factor

Orbital elements

Apogee altitude

37,061.433 km

Perigee altitude

3,313.874 km

Semi-major axis

26,565.79 km

Eccentricity

0.63517

Inclination

17.1632°

RAAN

122.0038°

Arg. of periapsis

59.5049°

True anomaly

Unknown

Mean anomaly

347.9589°

Eccentric anomaly

Unknown

Mean motion

0.50126 °/min

Orbital period

718.2 mins

BSTAR

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Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

DELTA 1 R/B(1), 2515 (Decayed)

DELTA 1 R/B(2) *, 11792

INTELSAT 2-F1 Visibility forecast

Observer location: undefined°, undefined°

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.
640 mins	2025-07-06 03:44:25.870Z	245.751° WSW	2025-07-06 04:01:25.870Z	178.687° S	33.507°	2025-07-06 14:24:25.870Z	141.217° SSE

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Check out INTELSAT 2-F1, 2514 on other resources

View INTELSAT 2-F1, 2514 on NASA - NSSDCA Website

View INTELSAT 2-F1, 2514 on Heavens-Above

View INTELSAT 2-F1, 2514 on Keep Track

View INTELSAT 2-F1, 2514 on Celestrak

View INTELSAT 2-F1, 2514 on Gunter's Space Page

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