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: 18 hours ago

TLE from 18 hours ago
0 ETS 6 DEB
1 23248U 94056C   26110.69119215 -.00000047  00000-0  00000-0 0  9999
2 23248  11.8600 147.7670 5174344 347.8386 190.1336  1.70301564196721
Epoch: 2026-04-20T16:35Z
TLE epoch observation values (Epoch: 2026-04-20T16:35:19.001Z)
Latitude
1.72535°
Longitude
-138.01563°
Altitude
38,433.544 km
Speed
2.082 km/s
True Right ascension
21h 18m 21s
True Declination
1° 43' 25"
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
17:16:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,572.122 km
Perigee altitude
7,916.681 km
Semi-major axis
29,622.538 km
Eccentricity
0.51743
Inclination
11.86°
RAAN
147.767°
Arg. of periapsis
347.8386°
True anomaly
183.7718°
Mean anomaly
190.1336°
Eccentric anomaly
186.68328°
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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