ETS 6 DEB, 23248

Orbit data source: Space-Track

ETS 6 DEB, 23248 is space debris in HEO originally from a launch on Sun, 28 Aug 1994 UTC launched from the Tanegashima Space Center (TNSTA). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
23248, 1994-056C
Orbit
HEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
IHI
Mission
Spacecraft
Bus & Motor
LAPS, Unknown motor
Mass
~1,844 kg wet, ~150 kg dry
Launch date (UTC)
1994-08-28 (32 years ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Dish + 2 Pan, 1.8 m
Radar Cross Section
12.600 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 ETS 6 DEB
1 23248U 94056C   26169.44813927 -.00000083  00000-0  00000+0 0  9996
2 23248  11.9869 142.4049 5164778 357.9703 212.8387  1.70301503197728
Epoch: 2026-06-18T10:45Z
TLE epoch observation values (Epoch: 2026-06-18T10:45:19.232Z)
Latitude
-2.14855°
Longitude
-95.47674°
Altitude
37,422.583 km
Speed
2.178 km/s
True Right ascension
22h 10m 10s
True Declination
-2° 08' 47"
Sunlit
Object was in daylight 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
11:29:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,543.784 km
Perigee altitude
7,945.018 km
Semi-major axis
29,622.538 km
Eccentricity
0.51648
Inclination
11.9869°
RAAN
142.4049°
Arg. of periapsis
357.9703°
True anomaly
192.43084°
Mean anomaly
212.8387°
Eccentric anomaly
201.83324°
Mean motion
0.42571 °/min
Orbital period
845.65 mins
BSTAR
0
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Other satellites on launch #56 in the year 1994 (1994-08-28 UTC)

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