INTELSAT II F-3

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Link to this page

https://orbinauts.com/satellites/2717

  • Communications satellite
  • INTELSAT 2-F3
  • NORAD 2717
  • 1967-026A
  • Geostationary

Current orbit

Where INTELSAT II F-3 is on the world map, with the orbit it is flying
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One orbit takes a day, as long as the Earth takes to turn, so INTELSAT II F-3 keeps above 86.4° E of the equator and never crosses the sky.

Past trackNext orbits

It never rises or sets

INTELSAT II F-3 turns with the Earth, standing over one longitude of the equator. From anywhere it can be seen at all it is up day and night, in the same direction, so there is no pass to wait for.

No brightness has been published for INTELSAT II F-3, so it is not a naked-eye satellite and no city page carries pass times for it. Nothing here estimates one.

Seeing it

There is nothing to wait for: it never crosses the sky. From the half of the Earth it stands over it keeps the same point day and night, and from the other half it never rises at all.

Timeline

  1. Launch

    Launched, on the day GCAT records. Source

Summary

Over the Indian Ocean LIVE

Where is INTELSAT II F-3?

At 5:36:41 PM UTC INTELSAT II F-3 was over the Indian Ocean (2.1° S, 86.4° E), 35,778 km up, standing over one longitude of the equator and in sunlight.

What is INTELSAT II F-3?

A communications satellite in geostationary orbit, in space since Mar 23, 1967.

Can I see INTELSAT II F-3?

No, not with the naked eye, and it never crosses the sky: INTELSAT II F-3 stands over 86.4° E of the equator; the dishes and receivers on the ground use its signals instead.

General

Operator
INTELSAT
State
International Telecommunications Satellite Organization
Built by
Hughes Space and Comms. Co (Hughes Satellite Systems)
What it is
Communications satellite
Launched
Mass
75 kg
Operating
Orbit class
Geostationary

From GCAT, Jonathan McDowell’s general catalogue, licensed CC BY 4.0: the operator, the state, the manufacturer, what it is for, the launch day, the mass, and whether it is operating. The orbit class is read from its current elements.

Latest orbital data

Position received
5:36 PM UTC
Station time (UTC)
5:36 PM UTC
Latitude / longitude
2.1° S, 86.4° E
Altitude
35,778 km
Speed
3.07 km/s (11,066 km/h)
Course
Stands over 86.4° E
Light
In sunlight
Inclination
4.4°
Orbital period
1,434.4 minutes
Orbits per day
1
This orbit
35,673 to 35,835 km
In view from
Within 7,940 km of the point below it
Elements epoch
Nov 7, 2026, 8:50 PM, 20 hours old
Source
Position from Space-Track orbital elements of Nov 7, 2026, 8:50 PM, 20 hours old.

No operator publishes an ephemeris for INTELSAT II F-3, so every position here comes from its orbital elements.

In orbit

Close approaches
No close approach to INTELSAT II F-3 has been reported publicly in the past thirty days.

From Space-Track’s public conjunction messages; the latest report was issued Nov 8, 2026, 1:11 PM, 3 hours old. Only approaches serious enough to be reported publicly are listed: within three days and, for two bodies near the Earth, closer than a kilometre with a chance of a collision above 1 in 10,000, the level at which NASA moves the ISS.

See every close approach reported in orbit.

Beside the others

SatelliteTypical altitudeOrbital periodMassIn space since
INTELSAT II F-335,673 to 35,835 km1,434 minutes75 kg1967
Hispasat 30W-635,786 to 35,786 km1,436 minutesabout 6.1 t2018
Amazonas Nexus35,786 to 35,786 km1,436 minutesabout 4.1 t2023
ARSAT-135,786 to 35,786 km1,436 minutesabout 3 t2014
Astra 1N35,786 to 35,786 km1,436 minutesabout 5.3 t2011
Hotbird 13F35,786 to 35,786 km1,436 minutesabout 4.5 t2022

Data and API

The current elements from Space-Track as an OMM object, epoch Nov 7, 2026, 8:50 PM, 20 hours old.

{
  "OBJECT_NAME": "INTELSAT 2-F3",
  "OBJECT_ID": "1967-026A",
  "EPOCH": "2026-11-07T20:50:38.711040",
  "MEAN_MOTION": 1.00391891,
  "ECCENTRICITY": 0.00191795,
  "INCLINATION": 4.4324,
  "RA_OF_ASC_NODE": 66.8534,
  "ARG_OF_PERICENTER": 223.4423,
  "MEAN_ANOMALY": 155.233,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 2717,
  "ELEMENT_SET_NO": 999,
  "REV_AT_EPOCH": 12534,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.00000212,
  "MEAN_MOTION_DDOT": 0
}