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 (31 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: 1 week ago

TLE from 1 week ago
0 ETS 6 DEB
1 23248U 94056C   26042.08725329 -.00000131  00000-0  00000-0 0  9999
2 23248  11.7177 154.2619 5192653 335.8049 250.6316  1.70299633195554
Epoch: 2026-02-11T02:05Z
TLE epoch observation values (Epoch: 2026-02-11T02:05:38.684Z)
Latitude
-0.86008°
Longitude
165.74236°
Altitude
33,479.737 km
Speed
2.558 km/s
True Right ascension
22h 33m 14s
True Declination
0° 51' 33"
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
19:07:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,626.716 km
Perigee altitude
7,862.559 km
Semi-major axis
29,622.774 km
Eccentricity
0.51927
Inclination
11.7177°
RAAN
154.2619°
Arg. of periapsis
335.8049°
True anomaly
208.36696°
Mean anomaly
250.6316°
Eccentric anomaly
228.3876°
Mean motion
0.4257 °/min
Orbital period
845.66 mins
BSTAR
0
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Other satellites on launch #56 in the year 1994 (1994-08-28 UTC)

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