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IHI-SAT2, 66772

Orbit data source: Space-Track

IHI-SAT2, 66772 is a payload satellite owned by IHI Corp (JP) in SSO that was launched on Fri, 28 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
66772, 2025-276DL
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
NanoAvionics
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2025-11-28 (9 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.055 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 IHI-SAT2
1 66772U 25276DL  26238.43734391  .00005380  00000-0  23721-3 0  9999
2 66772  97.4193 311.5446 0001439  49.0749 311.0611 15.22210882 41130
Epoch: 2026-08-26T10:29Z
TLE epoch observation values (Epoch: 2026-08-26T10:29:46.513Z)
Latitude
-0.00011°
Longitude
179.41046°
Altitude
501.616 km
Speed
7.614 km/s
True Right ascension
20h 46m 10s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
11:46:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.126 km
Perigee altitude
495.148 km
Semi-major axis
6,874.274 km
Eccentricity
0.00014
Inclination
97.4193°
RAAN
311.5446°
Arg. of periapsis
49.0749°
True anomaly
311.04867°
Mean anomaly
311.0611°
Eccentric anomaly
311.05488°
Mean motion
3.80805 °/min
Orbital period
94.54 mins
BSTAR
0.00023721
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