TEMPSAT 1
NORAD 1512
Payload
LEO
1965-065E
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LEO · NORAD 1512
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
1082 km
Apogee
1184 km
Inclination
90.0°
Period
108.0 min
Mean Motion
13.33600749 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,133 km
Orbital Velocity26,238 km/h
Velocity7.29 km/s
Orbital Period108 minutes
Orbits / Day13.34
Eccentricity0.0068
Semi-Major Axis7,504 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NRL (United States)
Launch Date
1965-08-13
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-065E
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TEMPSAT 1 is an active satellite operated by NRL (United States), launched on 1965-08-13 from Vandenberg Space Force Base, United States on the Dodecapole 2 launch. After more than 61 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 1,082 km and 1,184 km with an inclination of 90.0°. It travels at approximately 26,238 km/h (7.29 km/s), completing one full orbit every 108 minutes — that’s roughly 13.34 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Orbital Radar tracks TEMPSAT 1 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 1 orbits at an average altitude of 1,133 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 1’s average altitude, there are currently 394 active payloads and 438 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0250, ONEWEB-0321, ONEWEB-0334. With an inclination of 90.0°, TEMPSAT 1 passes over latitudes between 90.0°N and 90.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,279 active satellites in total, of which 31 share a similar altitude band with TEMPSAT 1.
❓ Frequently Asked Questions
TEMPSAT 1 orbits in Low Earth Orbit (LEO) at altitudes between 1,082 km (perigee) and 1,184 km (apogee), with an average altitude of approximately 1,133 km. It completes one orbit every 108 minutes, travelling at approximately 26,238 km/h (16,303 mph).
TEMPSAT 1 is operated by NRL (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 1512. You can track TEMPSAT 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TEMPSAT 1 was launched on 1965-08-13 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks TEMPSAT 1 (NORAD ID 1512) 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 1 travels at approximately 26,238 km/h (16,303 mph) — roughly 7.29 km/s. It completes 13.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.