OPS 9390
NORAD 6317
Payload
MEO
1972-101A
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MEO · NORAD 6317
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🛰️ Orbital Parameters
Perigee
30670 km
Apogee
40881 km
Inclination
8.9°
Period
1435.5 min
Mean Motion
1.00310525 rev/day
TLE Epoch
2026-10-21 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,776 km
Orbital Velocity11,071 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.1211
Semi-Major Axis42,147 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 NRO / SAFSP (United States)
Launch Date
1972-12-20
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1972-101A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 9390 is an active satellite operated by NRO / SAFSP (United States), launched on 1972-12-20 from Cape Canaveral Space Force Station, United States on the CANYON 5 launch. After more than 54 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 30,670 km and 40,881 km with an inclination of 8.9°. It travels at approximately 11,071 km/h (3.08 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. Its orbital eccentricity of 0.1211 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 9390 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 9390 orbits at an average altitude of 35,776 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 9390’s average altitude, there are currently 738 active payloads and 61 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. With an inclination of 8.9°, OPS 9390 passes over latitudes between 8.9°N and 8.9°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 13,276 active satellites in total, of which 157 share a similar altitude band with OPS 9390.
❓ Frequently Asked Questions
OPS 9390 orbits in Medium Earth Orbit (MEO) at altitudes between 30,670 km (perigee) and 40,881 km (apogee), with an average altitude of approximately 35,776 km. It completes one orbit every ~24 hours (geosynchronous), travelling at approximately 11,071 km/h (6,879 mph).
OPS 9390 is operated by NRO / SAFSP (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 6317. You can track OPS 9390 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 9390 was launched on 1972-12-20 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 9390 (NORAD ID 6317) 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 9390 travels at approximately 11,071 km/h (6,879 mph) — roughly 3.08 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.