USA 40 R/B DEB, 23388

Orbit data source: Space-Track

USA 40 R/B DEB, 23388 is space debris in LEO originally from a launch on Tue, 08 Aug 1989 UTC launched from the Air Force Eastern Test Range (AFETR). 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
23388, 1989-061BL
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1989-08-08 (37 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago
0 USA 40 R/B DEB
1 23388U 89061BL  26162.27961309  .00004830  00000-0  25035-2 0  9994
2 23388  56.9913  22.7843 2261465 243.7840  91.3773 10.35119776 82841
Epoch: 2026-06-11T06:42Z
TLE epoch observation values (Epoch: 2026-06-11T06:42:38.570Z)
Latitude
-0.00004°
Longitude
22.49788°
Altitude
3,001.227 km
Speed
6.34 km/s
True Right ascension
01h 31m 08s
True Declination
0° 00' 00"
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
02:18:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,526.295 km
Perigee altitude
503.939 km
Semi-major axis
8,893.254 km
Eccentricity
0.22615
Inclination
56.9913°
RAAN
22.7843°
Arg. of periapsis
243.784°
True anomaly
116.30178°
Mean anomaly
91.3773°
Eccentric anomaly
103.95226°
Mean motion
2.58793 °/min
Orbital period
139.11 mins
BSTAR
0.0025035
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