OPS 4682 DEB, 38388

Orbit data source: Space-Track

OPS 4682 DEB, 38388 is space debris in LEO originally from a launch on Sat, 03 Apr 1965 UTC launched from the Air Force Western Test Range (AFWTR). 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
38388, 1965-027CR
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-04-03 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 OPS 4682 DEB
1 38388U 65027CR  26104.18604385 -.00000467  00000-0 -15608-2 0  9999
2 38388  90.2720  21.4340 0033792 154.2101 206.0716 13.00615691655745
Epoch: 2026-04-14T04:27Z
TLE epoch observation values (Epoch: 2026-04-14T04:27:54.188Z)
Latitude
0.00005°
Longitude
112.0923°
Altitude
1,285.765 km
Speed
7.202 km/s
True Right ascension
01h 25m 44s
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
19:19:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,282.601 km
Perigee altitude
1,231.001 km
Semi-major axis
7,634.938 km
Eccentricity
0.00338
Inclination
90.272°
RAAN
21.434°
Arg. of periapsis
154.2101°
True anomaly
205.90206°
Mean anomaly
206.0716°
Eccentric anomaly
205.98677°
Mean motion
3.25338 °/min
Orbital period
110.65 mins
BSTAR
-0.0015608
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