OPS 4682 DEB, 38404

Orbit data source: Space-Track

OPS 4682 DEB, 38404 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
38404, 1965-027DH
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 week ago

TLE from 1 week ago
0 OPS 4682 DEB
1 38404U 65027DH  26066.51380065  .00000864  00000-0  28587-2 0  9997
2 38404  90.2458   4.0754 0018276 209.4415 150.5679 12.99699377651612
Epoch: 2026-03-07T12:19Z
TLE epoch observation values (Epoch: 2026-03-07T12:19:52.376Z)
Latitude
-0°
Longitude
13.8728°
Altitude
1,278.319 km
Speed
7.211 km/s
True Right ascension
00h 16m 18s
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
07:31:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,274.352 km
Perigee altitude
1,246.432 km
Semi-major axis
7,638.529 km
Eccentricity
0.00183
Inclination
90.2458°
RAAN
4.0754°
Arg. of periapsis
209.4415°
True anomaly
150.67061°
Mean anomaly
150.5679°
Eccentric anomaly
150.61927°
Mean motion
3.25109 °/min
Orbital period
110.73 mins
BSTAR
0.0028587
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