TDRS 1
NORAD 13969
Payload
GEO
1983-026B
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GEO · NORAD 13969
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
36137 km
Apogee
36302 km
Inclination
8.7°
Period
1458.3 min
Mean Motion
0.98745833 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,220 km
Orbital Velocity11,013 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0019
Semi-Major Axis42,591 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 NASA (United States)
Launch Date
1983-04-04
Launch Site
Cape Canaveral, Florida
Int'l Designator
1983-026B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TDRS 1 is an active satellite operated by NASA (United States), launched on 1983-04-04 from Cape Canaveral, Florida. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,137 km and 36,302 km with an inclination of 8.7°. It travels at approximately 11,013 km/h (3.06 km/s), completing one full orbit every 24.3 hours — that’s roughly 0.99 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 TDRS 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TDRS 1 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 8.7°, 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 TDRS 1’s average altitude, there are currently 85 active payloads and 18 tracked debris or rocket body fragments. United States operates approximately 12,360 active satellites in total, of which 29 share a similar altitude band with TDRS 1.
🔗 Tracking and Data Relay Satellite System
This satellite is part of NASA's Tracking and Data Relay Satellite System (TDRSS), a network of GEO communications satellites that provides continuous high-bandwidth contact with the ISS, Hubble, scientific spacecraft and launch vehicles. TDRS eliminates coverage gaps that would exist with ground stations alone, enabling near-global real-time telemetry and command relay.
❓ Frequently Asked Questions
TDRS 1 orbits at approximately 36,220 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 11,013 km/h — it just keeps pace with the ground below. With an inclination of 8.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
TDRS 1 is operated by NASA (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13969. You can track TDRS 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TDRS 1 was launched on 1983-04-04 from Cape Canaveral, Florida, 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 TDRS 1 (NORAD ID 13969) 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.
TDRS 1 travels at approximately 11,013 km/h (6,843 mph) — roughly 3.06 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.