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INTELSAT 2-F1

NORAD 2514 Payload MEO 1966-096A ● Active
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🛰️ Orbital Parameters
Perigee
3217 km
Apogee
37191 km
Inclination
18.4°
Period
718.9 min
Mean Motion
2.00314618 rev/day
TLE Epoch
2026-10-21 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,204 km
Orbital Velocity13,942 km/h
Velocity3.87 km/s
Orbital Period11 hours 59 minutes
Orbits / Day2.00
Eccentricity0.6392
Semi-Major Axis26,575 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
INTELSAT (ITSO)
Launch Date
1966-10-26
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1966-096A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
intelsat
📖 About This Object
INTELSAT 2-F1 is an active satellite operated by INTELSAT (ITSO), launched on 1966-10-26 from Cape Canaveral Space Force Station, United States on the INTELSAT II F-1 launch. After more than 60 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 3,217 km and 37,191 km with an inclination of 18.4°. It travels at approximately 13,942 km/h (3.87 km/s), completing one full orbit every 11 hours 59 minutes — that’s roughly 2.00 orbits per day. Its orbital eccentricity of 0.6392 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. It is part of the Intelsat constellation group. Orbital Radar tracks INTELSAT 2-F1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
INTELSAT 2-F1 orbits at an average altitude of 20,204 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of INTELSAT 2-F1’s average altitude, there are currently 106 active payloads and 16 tracked debris or rocket body fragments. With an inclination of 18.4°, INTELSAT 2-F1 passes over latitudes between 18.4°N and 18.4°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. ITSO operates approximately 91 active satellites in total.
🔗 Intelsat Communications

This satellite is operated by Intelsat, one of the pioneering commercial satellite operators, with a fleet of 50+ geostationary satellites providing television distribution, enterprise networking, mobility connectivity and government communications worldwide. Intelsat was founded in 1964 as an intergovernmental organisation and privatised in 2001.

❓ Frequently Asked Questions
INTELSAT 2-F1 orbits in Medium Earth Orbit (MEO) at altitudes between 3,217 km (perigee) and 37,191 km (apogee), with an average altitude of approximately 20,204 km. It completes one orbit every 11 hours 59 minutes, travelling at approximately 13,942 km/h (8,663 mph).
INTELSAT 2-F1 is operated by INTELSAT (ITSO). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2514. You can track INTELSAT 2-F1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INTELSAT 2-F1 was launched on 1966-10-26 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks INTELSAT 2-F1 (NORAD ID 2514) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
INTELSAT 2-F1 travels at approximately 13,942 km/h (8,663 mph) — roughly 3.87 km/s. It completes 2.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.
INTELSAT 2-F1 is a member of the Intelsat constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Intelsat satellites on Orbital Radar’s live tracker.