TEMPSAT 2
NORAD 4168
Payload
LEO
1969-082H
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LEO · NORAD 4168
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
892 km
Apogee
923 km
Inclination
70.0°
Period
103.2 min
Mean Motion
13.96029387 rev/day
TLE Epoch
2026-10-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude908 km
Orbital Velocity26,641 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.96
Eccentricity0.0021
Semi-Major Axis7,279 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NRL (United States)
Launch Date
1969-09-30
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1969-082H
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TEMPSAT 2 is an active satellite operated by NRL (United States), launched on 1969-09-30 from Vandenberg Space Force Base, United States on the P-11 No. 4407 launch. After more than 57 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 892 km and 923 km with an inclination of 70.0°. It travels at approximately 26,641 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.96 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks TEMPSAT 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
TEMPSAT 2 orbits at an average altitude of 908 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 TEMPSAT 2’s average altitude, there are currently 309 active payloads and 1,539 tracked debris or rocket body fragments. With an inclination of 70.0°, TEMPSAT 2 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 151 share a similar altitude band with TEMPSAT 2.
❓ Frequently Asked Questions
TEMPSAT 2 orbits in Low Earth Orbit (LEO) at altitudes between 892 km (perigee) and 923 km (apogee), with an average altitude of approximately 908 km. It completes one orbit every 103 minutes, travelling at approximately 26,641 km/h (16,554 mph).
TEMPSAT 2 is operated by NRL (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 4168. You can track TEMPSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TEMPSAT 2 was launched on 1969-09-30 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 TEMPSAT 2 (NORAD ID 4168) 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.
TEMPSAT 2 travels at approximately 26,641 km/h (16,554 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.