OPS 4682 DEB, 38402

Orbit data source: Space-Track

OPS 4682 DEB, 38402 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
38402, 1965-027DF
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1965-04-03 (62 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.062 m
Radar Cross Section
Small (<0.1 m²)

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

TLE from 2 days ago
0 OPS 4682 DEB
1 38402U 65027DF  26296.18642730  .00000301  00000-0  10651-2 0  9992
2 38402  90.2474   7.8978 0025187 286.7831  73.0524 12.93939136603648
Epoch: 2026-10-23T04:28Z
TLE epoch observation values (Epoch: 2026-10-23T04:28:27.318Z)
Latitude
-0.0001°
Longitude
-90.82661°
Altitude
1,283.217 km
Speed
7.217 km/s
True Right ascension
00h 31m 35s
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
15:26:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,302.358 km
Perigee altitude
1,263.766 km
Semi-major axis
7,661.199 km
Eccentricity
0.00252
Inclination
90.2474°
RAAN
7.8978°
Arg. of periapsis
286.7831°
True anomaly
73.32874°
Mean anomaly
73.0524°
Eccentric anomaly
73.19054°
Mean motion
3.23667 °/min
Orbital period
111.23 mins
BSTAR
0.0010651
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