SECOR 1B
NORAD 729
Payload
LEO
1964-001C
● Active
CONNECTING…
LEO · NORAD 729
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
898 km
Apogee
923 km
Inclination
69.9°
Period
103.2 min
Mean Motion
13.95236728 rev/day
TLE Epoch
2026-10-21 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude911 km
Orbital Velocity26,636 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.95
Eccentricity0.0017
Semi-Major Axis7,282 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 USA ACE / GIMRADA (United States)
Launch Date
1964-01-11
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1964-001C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SECOR 1B is an active satellite operated by USA ACE / GIMRADA (United States), launched on 1964-01-11 from Vandenberg Space Force Base, United States on the POPPY 3/HAYLOFT launch. After more than 62 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 898 km and 923 km with an inclination of 69.9°. It travels at approximately 26,636 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.95 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks SECOR 1B in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SECOR 1B orbits at an average altitude of 911 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 SECOR 1B’s average altitude, there are currently 311 active payloads and 1,498 tracked debris or rocket body fragments. With an inclination of 69.9°, SECOR 1B passes over latitudes between 69.9°N and 69.9°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 153 share a similar altitude band with SECOR 1B.
❓ Frequently Asked Questions
SECOR 1B orbits in Low Earth Orbit (LEO) at altitudes between 898 km (perigee) and 923 km (apogee), with an average altitude of approximately 911 km. It completes one orbit every 103 minutes, travelling at approximately 26,636 km/h (16,551 mph).
SECOR 1B is operated by USA ACE / GIMRADA (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 729. You can track SECOR 1B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SECOR 1B was launched on 1964-01-11 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 SECOR 1B (NORAD ID 729) 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.
SECOR 1B travels at approximately 26,636 km/h (16,551 mph) — roughly 7.40 km/s. It completes 13.95 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.