OPS 4682 DEB, 38427

Orbit data source: Space-Track

OPS 4682 DEB, 38427 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
38427, 1965-027EG
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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago
0 OPS 4682 DEB
1 38427U 65027EG  26258.27643577 -.00000983  00000-0 -37129-2 0  9994
2 38427  90.2364   2.5210 0028687 308.7155  51.1398 12.91356100673371
Epoch: 2026-09-15T06:38Z
TLE epoch observation values (Epoch: 2026-09-15T06:38:04.050Z)
Latitude
0.00001°
Longitude
-91.24058°
Altitude
1,285.237 km
Speed
7.22 km/s
True Right ascension
00h 10m 05s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
06:08:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,315.29 km
Perigee altitude
1,271.276 km
Semi-major axis
7,671.42 km
Eccentricity
0.00287
Inclination
90.2364°
RAAN
2.521°
Arg. of periapsis
308.7155°
True anomaly
51.39635°
Mean anomaly
51.1398°
Eccentric anomaly
51.26802°
Mean motion
3.2302 °/min
Orbital period
111.45 mins
BSTAR
-0.0037129
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