KIKU 2 (ETS 2)
NORAD 9852
Payload
GEO
1977-014A
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🛰️ Orbital Parameters
Perigee
35851 km
Apogee
35863 km
Inclination
5.0°
Period
1439.7 min
Mean Motion
1.00020401 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,857 km
Orbital Velocity11,060 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0001
Semi-Major Axis42,228 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 NASDA (Japan)
Launch Date
1977-02-23
Launch Site
Tanegashima Space Center, Japan
Int'l Designator
1977-014A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
KIKU 2 (ETS 2) is an active satellite operated by NASDA (Japan), launched on 1977-02-23 from Tanegashima Space Center, Japan on the ETS-2 launch. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,851 km and 35,863 km with an inclination of 5.0°. It travels at approximately 11,060 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 KIKU 2 (ETS 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
KIKU 2 (ETS 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 5.0°, 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 KIKU 2 (ETS 2)’s average altitude, there are currently 74 active payloads and 48 tracked debris or rocket body fragments. Japan operates approximately 209 active satellites in total.
❓ Frequently Asked Questions
KIKU 2 (ETS 2) orbits at approximately 35,857 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 11,060 km/h — it just keeps pace with the ground below. With an inclination of 5.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
KIKU 2 (ETS 2) is operated by NASDA (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 9852. You can track KIKU 2 (ETS 2) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
KIKU 2 (ETS 2) was launched on 1977-02-23 from Tanegashima Space Center, Japan, Japan’s primary launch site, operated by JAXA on a small island south of Kyushu. View the full satellite launch log.
Yes — Orbital Radar tracks KIKU 2 (ETS 2) (NORAD ID 9852) 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.
KIKU 2 (ETS 2) travels at approximately 11,060 km/h (6,873 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.