OPS 1948
NORAD 11558
Payload
MEO
1979-086A
● Active
CONNECTING…
MEO · NORAD 11558
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
30266 km
Apogee
41363 km
Inclination
6.0°
Period
1437.5 min
Mean Motion
1.00173684 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,815 km
Orbital Velocity11,066 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.1315
Semi-Major Axis42,186 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1979-10-01
Launch Site
Cape Canaveral, Florida
Int'l Designator
1979-086A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 1948 is an active satellite operated by United States, launched on 1979-10-01 from Cape Canaveral, Florida. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 30,266 km and 41,363 km with an inclination of 6.0°. It travels at approximately 11,066 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. Its orbital eccentricity of 0.1315 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks OPS 1948 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 1948 orbits at an average altitude of 35,815 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 OPS 1948’s average altitude, there are currently 710 active payloads and 66 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. With an inclination of 6.0°, OPS 1948 passes over latitudes between 6.0°N and 6.0°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 12,360 active satellites in total, of which 142 share a similar altitude band with OPS 1948.
❓ Frequently Asked Questions
OPS 1948 orbits in Medium Earth Orbit (MEO) at altitudes between 30,266 km (perigee) and 41,363 km (apogee), with an average altitude of approximately 35,815 km. It completes one orbit every ~24 hours (geosynchronous), travelling at approximately 11,066 km/h (6,876 mph).
OPS 1948 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 11558. You can track OPS 1948 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 1948 was launched on 1979-10-01 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 OPS 1948 (NORAD ID 11558) 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.
OPS 1948 travels at approximately 11,066 km/h (6,876 mph) — roughly 3.07 km/s. It completes 1.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.