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OPS 1948

NORAD 11558 Payload MEO 1979-086A ● Active
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🛰️ Orbital Parameters
Perigee
30286 km
Apogee
41316 km
Inclination
6.1°
Period
1436.8 min
Mean Motion
1.00219789 rev/day
TLE Epoch
2026-11-02 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,801 km
Orbital Velocity11,068 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.1308
Semi-Major Axis42,172 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 NRO / SAFSP (United States)
Launch Date
1979-10-01
Launch Site
Cape Canaveral Space Force Station, United States
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 NRO / SAFSP (United States), launched on 1979-10-01 from Cape Canaveral Space Force Station, United States on the VORTEX 2 launch. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 30,286 km and 41,316 km with an inclination of 6.1°. It travels at approximately 11,068 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 0.1308 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 35,801 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 733 active payloads and 66 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. With an inclination of 6.1°, OPS 1948 passes over latitudes between 6.1°N and 6.1°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 13,340 active satellites in total, of which 154 share a similar altitude band with OPS 1948.
❓ Frequently Asked Questions
OPS 1948 orbits in Medium Earth Orbit (MEO) at altitudes between 30,286 km (perigee) and 41,316 km (apogee), with an average altitude of approximately 35,801 km. It completes one orbit every ~24 hours (geosynchronous), travelling at approximately 11,068 km/h (6,877 mph).
OPS 1948 is operated by NRO / SAFSP (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 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 1948 (NORAD ID 11558) 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 1948 travels at approximately 11,068 km/h (6,877 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.