SMS 2
NORAD 7648
Payload
GEO
1975-011A
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GEO · NORAD 7648
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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
35939 km
Apogee
36066 km
Inclination
5.2°
Period
1447.1 min
Mean Motion
0.99506981 rev/day
TLE Epoch
2026-10-21 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,003 km
Orbital Velocity11,041 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0015
Semi-Major Axis42,374 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 GSFC (United States)
Launch Date
1975-02-06
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1975-011A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SMS 2 is an active satellite operated by GSFC (United States), launched on 1975-02-06 from Cape Canaveral Space Force Station, United States on the SMS B launch. After more than 51 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 35,939 km and 36,066 km with an inclination of 5.2°. It travels at approximately 11,041 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 SMS 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SMS 2 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 5.2°, 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 SMS 2’s average altitude, there are currently 66 active payloads and 33 tracked debris or rocket body fragments. United States operates approximately 13,276 active satellites in total, of which 20 share a similar altitude band with SMS 2.
❓ Frequently Asked Questions
SMS 2 orbits at approximately 36,003 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 11,041 km/h — it just keeps pace with the ground below. With an inclination of 5.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
SMS 2 is operated by GSFC (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 7648. You can track SMS 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SMS 2 was launched on 1975-02-06 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 SMS 2 (NORAD ID 7648) 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.
SMS 2 travels at approximately 11,041 km/h (6,861 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.