Skip to content
Home Library Satellite Directory NSTAR C

NSTAR C

NORAD 27461 Payload GEO 2002-035B ● Active
CONNECTING… GEO · NORAD 27461
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
36135 km
Apogee
36185 km
Inclination
11.1°
Period
1455.2 min
Mean Motion
0.98955230 rev/day
TLE Epoch
2026-06-19 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,160 km
Orbital Velocity11,021 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0006
Semi-Major Axis42,531 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2002-07-05
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2002-035B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
NSTAR C is an active satellite operated by Japan, launched on 2002-07-05 from Guiana Space Centre, Kourou. With over 24 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,135 km and 36,185 km with an inclination of 11.1°. It travels at approximately 11,021 km/h (3.06 km/s), completing one full orbit every 24.3 hours — that’s roughly 0.99 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 NSTAR C in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
NSTAR C 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 11.1°, 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 NSTAR C’s average altitude, there are currently 163 active payloads and 9 tracked debris or rocket body fragments. Japan operates approximately 189 active satellites in total, of which 17 share a similar altitude band with NSTAR C.
❓ Frequently Asked Questions
NSTAR C orbits at approximately 36,160 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 11,021 km/h — it just keeps pace with the ground below. With an inclination of 11.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
NSTAR C is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27461. You can track NSTAR C in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
NSTAR C was launched on 2002-07-05 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. View the full satellite launch log.
Yes — Orbital Radar tracks NSTAR C (NORAD ID 27461) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. 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.
NSTAR C travels at approximately 11,021 km/h (6,848 mph) — roughly 3.06 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.