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Home Library Satellite Directory TELSTAR 4 (TELSTAR 402R)

TELSTAR 4 (TELSTAR 402R)

NORAD 23670 Payload GEO 1995-049A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35774 km
Apogee
35796 km
Inclination
13.6°
Period
1436.0 min
Mean Motion
1.00278765 rev/day
TLE Epoch
2026-06-19 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,785 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0003
Semi-Major Axis42,156 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1995-09-24
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1995-049A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TELSTAR 4 (TELSTAR 402R) is an active satellite operated by United States, launched on 1995-09-24 from Guiana Space Centre, Kourou. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,774 km and 35,796 km with an inclination of 13.6°. It travels at approximately 11,070 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks TELSTAR 4 (TELSTAR 402R) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TELSTAR 4 (TELSTAR 402R) occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 13.6°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of TELSTAR 4 (TELSTAR 402R)’s average altitude, there are currently 712 active payloads and 59 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United States operates approximately 12,360 active satellites in total, of which 146 share a similar altitude band with TELSTAR 4 (TELSTAR 402R).
❓ Frequently Asked Questions
TELSTAR 4 (TELSTAR 402R) orbits at approximately 35,785 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,070 km/h — it just keeps pace with the ground below. With an inclination of 13.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
TELSTAR 4 (TELSTAR 402R) is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23670. You can track TELSTAR 4 (TELSTAR 402R) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TELSTAR 4 (TELSTAR 402R) was launched on 1995-09-24 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. View the full satellite launch log.
Yes — Orbital Radar tracks TELSTAR 4 (TELSTAR 402R) (NORAD ID 23670) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. 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.
TELSTAR 4 (TELSTAR 402R) travels at approximately 11,070 km/h (6,878 mph) — roughly 3.07 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.