GGSE 5
NORAD 2834
Payload
LEO
1967-053D
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LEO · NORAD 2834
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
903 km
Apogee
911 km
Inclination
70.0°
Period
103.1 min
Mean Motion
13.96203352 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude907 km
Orbital Velocity26,642 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.96
Eccentricity0.0005
Semi-Major Axis7,278 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NRO / NRL (United States)
Launch Date
1967-05-31
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1967-053D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GGSE 5 is an active satellite operated by NRO / NRL (United States), launched on 1967-05-31 from Vandenberg Space Force Base, United States on the NRL PL160 launch. After more than 59 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 903 km and 911 km with an inclination of 70.0°. It travels at approximately 26,642 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.96 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks GGSE 5 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GGSE 5 orbits at an average altitude of 907 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of GGSE 5’s average altitude, there are currently 309 active payloads and 1,561 tracked debris or rocket body fragments. With an inclination of 70.0°, GGSE 5 passes over latitudes between 70.0°N and 70.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 13,279 active satellites in total, of which 150 share a similar altitude band with GGSE 5.
❓ Frequently Asked Questions
GGSE 5 orbits in Low Earth Orbit (LEO) at altitudes between 903 km (perigee) and 911 km (apogee), with an average altitude of approximately 907 km. It completes one orbit every 103 minutes, travelling at approximately 26,642 km/h (16,555 mph).
GGSE 5 is operated by NRO / NRL (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2834. You can track GGSE 5 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GGSE 5 was launched on 1967-05-31 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks GGSE 5 (NORAD ID 2834) 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.
GGSE 5 travels at approximately 26,642 km/h (16,555 mph) — roughly 7.40 km/s. It completes 13.96 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.