OPS 4682 DEB, 38392

Orbit data source: Space-Track

OPS 4682 DEB, 38392 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
38392, 1965-027CV
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: 2 weeks ago

TLE from 2 weeks ago
0 OPS 4682 DEB
1 38392U 65027CV  26198.19794035 -.00000037  00000-0 -15770-3 0  9994
2 38392  90.2489  14.0823 0032220  91.3047 269.1764 12.95333457615021
Epoch: 2026-07-17T04:45Z
TLE epoch observation values (Epoch: 2026-07-17T04:45:02.046Z)
Latitude
-0°
Longitude
7.79528°
Altitude
1,283.736 km
Speed
7.214 km/s
True Right ascension
00h 56m 19s
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
14:15:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,302.226 km
Perigee altitude
1,252.893 km
Semi-major axis
7,655.696 km
Eccentricity
0.00322
Inclination
90.2489°
RAAN
14.0823°
Arg. of periapsis
91.3047°
True anomaly
268.80725°
Mean anomaly
269.1764°
Eccentric anomaly
268.99182°
Mean motion
3.24016 °/min
Orbital period
111.11 mins
BSTAR
-0.0001577
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