Showing default

HORN-L, 69505

Orbit data source: Space-Track

HORN-L, 69505 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.

Loading next visibility...
Identifier
69505, 2026-132D
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: 2 days ago

TLE from 2 days ago
0 HORN-L
1 69505U 26132D   26191.59874568  .00002811  00000-0  16993-3 0  9993
2 69505  97.6828 255.1999 0028853 224.9163 134.9732 15.11180435  4305
Epoch: 2026-07-10T14:22Z
TLE epoch observation values (Epoch: 2026-07-10T14:22:11.626Z)
Latitude
-0.00005°
Longitude
111.12745°
Altitude
549.794 km
Speed
7.579 km/s
True Right ascension
17h 00m 47s
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
20:44:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.519 km
Perigee altitude
509.658 km
Semi-major axis
6,907.725 km
Eccentricity
0.00289
Inclination
97.6828°
RAAN
255.1999°
Arg. of periapsis
224.9163°
True anomaly
135.20651°
Mean anomaly
134.9732°
Eccentric anomaly
135.08991°
Mean motion
3.78042 °/min
Orbital period
95.23 mins
BSTAR
0.00016993
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #132 in the year 2026 (2026-06-12 UTC)

Documentation

Showing up to 5 results
|