Skip to content
Home › Library › Satellite Directory › ABS 1A (KOREASAT 2)

ABS 1A (KOREASAT 2)

NORAD 23768 Payload GEO 1996-003A ● Active
CONNECTING… GEO · NORAD 23768
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35906 km
Apogee
35938 km
Inclination
12.8°
Period
1443.0 min
Mean Motion
0.99789995 rev/day
TLE Epoch
2026-11-01 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,922 km
Orbital Velocity11,052 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0004
Semi-Major Axis42,293 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇰🇷 KTEL (South Korea)
Launch Date
1996-01-14
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1996-003A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ABS 1A (KOREASAT 2) is an active satellite operated by KTEL (South Korea), launched on 1996-01-14 from Cape Canaveral Space Force Station, United States on the Koreasat 2 launch. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,906 km and 35,938 km with an inclination of 12.8°. It travels at approximately 11,052 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks ABS 1A (KOREASAT 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
ABS 1A (KOREASAT 2) occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 12.8°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of ABS 1A (KOREASAT 2)’s average altitude, there are currently 75 active payloads and 17 tracked debris or rocket body fragments. South Korea operates approximately 65 active satellites in total, of which 3 share a similar altitude band with ABS 1A (KOREASAT 2).
❓ Frequently Asked Questions
ABS 1A (KOREASAT 2) orbits at approximately 35,922 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,052 km/h — it just keeps pace with the ground below. With an inclination of 12.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ABS 1A (KOREASAT 2) is operated by KTEL (South Korea). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23768. You can track ABS 1A (KOREASAT 2) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ABS 1A (KOREASAT 2) was launched on 1996-01-14 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 ABS 1A (KOREASAT 2) (NORAD ID 23768) 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.
ABS 1A (KOREASAT 2) travels at approximately 11,052 km/h (6,867 mph) — roughly 3.07 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.