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CHUBUSAT 2

NORAD 41338 Payload LEO 2016-012B ● Active
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🛰️ Orbital Parameters
Perigee
494 km
Apogee
505 km
Inclination
31.0°
Period
94.6 min
Mean Motion
15.22086175 rev/day
TLE Epoch
2026-11-01 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude500 km
Orbital Velocity27,421 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.22
Eccentricity0.0008
Semi-Major Axis6,871 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Nagoya (Japan)
Launch Date
2016-02-17
Launch Site
Tanegashima Space Center, Japan
Int'l Designator
2016-012B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CHUBUSAT 2 is an active satellite operated by Nagoya (Japan), launched on 2016-02-17 from Tanegashima Space Center, Japan on the ASTRO-H launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 494 km and 505 km with an inclination of 31.0°. It travels at approximately 27,421 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.22 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks CHUBUSAT 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
CHUBUSAT 2 orbits at an average altitude of 500 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of CHUBUSAT 2’s average altitude, there are currently 10,642 active payloads and 237 tracked debris or rocket body fragments — notable neighbours include STARLINK-1039, STARLINK-1184, STARLINK-1231. This makes it one of the more crowded altitude bands, containing roughly 56.1% of all active satellites. With an inclination of 31.0°, CHUBUSAT 2 passes over latitudes between 31.0°N and 31.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Japan operates approximately 207 active satellites in total, of which 31 share a similar altitude band with CHUBUSAT 2.
❓ Frequently Asked Questions
CHUBUSAT 2 orbits in Low Earth Orbit (LEO) at altitudes between 494 km (perigee) and 505 km (apogee), with an average altitude of approximately 500 km. It completes one orbit every 95 minutes, travelling at approximately 27,421 km/h (17,038 mph).
CHUBUSAT 2 is operated by Nagoya (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 41338. You can track CHUBUSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHUBUSAT 2 was launched on 2016-02-17 from Tanegashima Space Center, Japan, Japan’s primary launch site, operated by JAXA on a small island south of Kyushu. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CHUBUSAT 2 (NORAD ID 41338) 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.
CHUBUSAT 2 travels at approximately 27,421 km/h (17,038 mph) — roughly 7.62 km/s. It completes 15.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.