INTELSAT 2-F4

Satellite information

Favourite Embed

Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite INTELSAT 2-F4 at a glance.

Uptime

21211

Days in orbit

Revolutions

≈ 1.0

Per day

Orbit

GEO

Geostationary Orbit

Inclination

3.5

Latest

Satellite identification and parameters

Extended collection of information and parameters for INTELSAT 2-F4.

Object identification

Identified? True

Debris? False

Object name: INTELSAT 2-F4

International designator: 1967-094A

Object number (NORAD): 2969

Object ID (CCSDS): 2969

Country: INTERNATIONAL TELECOMMUNICATIONS SATELLITE ORGANIZATION (INTELSAT) (ITSO)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 1435.254 minutes

Inclination: 3.4721 deg

SMA: 42148.235 km

Apoapsis: 35828.179 km

Periapsis: 35712.022 km

RAAN: 76.6241 deg

Eccentricy: 0.00137795

Argument of periapsis: 140.7107 deg

Mean anomaly: 282.1557 deg

Mean motion: 1.00330659 rev/day

Mean motion (dot): 0.00000148 rev/day2

B* drag term: 0.0 1/REarth

Two-line elements (TLE)

Creation date: Oct. 24, 2025, 2:48 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 23, 2025, 5:33 p.m. UTC

TLE line 0: 0 INTELSAT 2-F4

TLE line 1: 1 02969U 67094A 25296.73168756 .00000148 00000-0 00000-0 0 9992

TLE line 2: 2 02969 3.4721 76.6241 0013780 140.7107 282.1557 1.00330659112944

Live tracking on map

Real-time ground track for satellite INTELSAT 2-F4.

In-orbit conjunctions

A list of the most updated potential collisions computed for object INTELSAT 2-F4.

Target Orbit TCA Probability of collision Miss distance Type
SL-12 R/B(2) OTHER 2025-10-26 14:57:00 TBA 2211.0 (m) ROCKET BODY
INTELSAT 33E DEB GEO 2025-06-30 10:05:56 TBA 4613.0 (m) DEBRIS
SL-12 R/B(2) OTHER 2024-11-23 14:39:01 TBA 4870.0 (m) ROCKET BODY

Associated space launch

The Intelsat II series of satellites, first launched in 1966, marked the third generation of communications satellites developed by Hughes.

INTELSAT 2-F4 was lifted into orbit during the mission ‘Thor Delta E1 | INTELSAT II F-4’, on board a Thor Delta E1 space rocket.

The launch took place on Sept. 28, 1967, 12:45 a.m. from Space Launch Complex 17B.

For more information about the launch, click the button.

Launch to space Thor Delta E1 | INTELSAT II F-4
Thor Delta E1 | INTELSAT II F-4

Agency: N/A

Status: Launch Successful

Launch date: Sept. 28, 1967, 12:45 a.m. UTC

Rocket: Thor Delta E1

Launch pad: Space Launch Complex 17B

Location: Cape Canaveral SFS, FL, USA

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.