OPS 9434 (DSCS 2-4)
NORAD 6974
Payload
GEO
1973-100B
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GEO · NORAD 6974
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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
36300 km
Apogee
36852 km
Inclination
4.4°
Period
1476.6 min
Mean Motion
0.97519583 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,576 km
Orbital Velocity10,967 km/h
Velocity3.05 km/s
Orbital Period24.6 hours
Orbits / Day0.98
Eccentricity0.0064
Semi-Major Axis42,947 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 SAMSO / US DCA (United States)
Launch Date
1973-12-13
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1973-100B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 9434 (DSCS 2-4) is an active satellite operated by SAMSO / US DCA (United States), launched on 1973-12-13 from Cape Canaveral Space Force Station, United States on the DSCS II B-3 launch. After more than 53 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 36,300 km and 36,852 km with an inclination of 4.4°. It travels at approximately 10,967 km/h (3.05 km/s), completing one full orbit every 24.6 hours — that’s roughly 0.98 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 OPS 9434 (DSCS 2-4) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OPS 9434 (DSCS 2-4) 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 4.4°, 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 OPS 9434 (DSCS 2-4)’s average altitude, there are currently 9 active payloads and 14 tracked debris or rocket body fragments. United States operates approximately 13,279 active satellites in total, of which 5 share a similar altitude band with OPS 9434 (DSCS 2-4).
❓ Frequently Asked Questions
OPS 9434 (DSCS 2-4) orbits at approximately 36,576 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 10,967 km/h — it just keeps pace with the ground below. With an inclination of 4.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
OPS 9434 (DSCS 2-4) is operated by SAMSO / US DCA (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 6974. You can track OPS 9434 (DSCS 2-4) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 9434 (DSCS 2-4) was launched on 1973-12-13 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 OPS 9434 (DSCS 2-4) (NORAD ID 6974) 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.
OPS 9434 (DSCS 2-4) travels at approximately 10,967 km/h (6,815 mph) — roughly 3.05 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.