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HORN-R, 69507

Orbit data source: Space-Track

HORN-R, 69507 is a Japanese payload satellite in SSO that was launched on Fri, 12 Jun 2026 UTC via a H3-30S launch vehicle from the Tanegashima Space Center (TNSTA). 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
69507, 2026-132F
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
BULL
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
11 kg wet, 11 kg dry
Launch date (UTC)
2026-06-12 (1 month ago)
Launch vehicle
H3-30S
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 5.9 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 HORN-R
1 69507U 26132F   26193.03617388  .00000519  00000-0  40121-4 0  9995
2 69507  97.6866 256.5489 0018099 216.9812 143.0168 15.05776636  4504
Epoch: 2026-07-12T00:52Z
TLE epoch observation values (Epoch: 2026-07-12T00:52:05.423Z)
Latitude
-0.00002°
Longitude
-46.4145°
Altitude
562.211 km
Speed
7.575 km/s
True Right ascension
17h 06m 11s
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
20:43:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.652 km
Perigee altitude
533.587 km
Semi-major axis
6,924.257 km
Eccentricity
0.00181
Inclination
97.6866°
RAAN
256.5489°
Arg. of periapsis
216.9812°
True anomaly
143.14134°
Mean anomaly
143.0168°
Eccentric anomaly
143.07909°
Mean motion
3.76689 °/min
Orbital period
95.57 mins
BSTAR
0.000040121
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Other satellites on launch #132 in the year 2026 (2026-06-12 UTC)

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